GRIMES AEROSPACE COMPANY

A WHOLLY OWNED SUBSIDIARY OF HONEYWELL INTERNATIONAL

550 STATE ROUTE 55
URBANA, OHIO 43078

TO: HOLDERS OF COMPONENT MAINTENANCE MANUAL 33-50-42 FOR THE EMERGENCY EXIT
LIGHT POWER SUPPLY, PART NUMBERS 60-1321-1, -1LB, -5, -5LB, -7, AND -7LB.

REVISION NO. 4 DATED FEBRUARY 1/06

HIGHLIGHTS

Pages which have been added or revised are outlined below together with the highlights of the revision.
Remove and insert the affected pages as listed and enter Revision No. 4 dated Feb 1/06 on the Record of
Revisions Sheet.

Page No. Description of Change Effectivity

T-1 Revised date. All Models

RR-1 Revised to reflect this revision. All Models

SBL-1 Revised to reflect this revision. All Models

LEP-1, -2 Revised to reflect this revision. All Models

1 Updated Figure 1 to show new labeling. All Models

101 Changed Part/Model Number for Variable Regulated Power Supplies to All Models
Commercially Available.

301 Moved step for removal of instruction plate to Repair section. All Models

401 Added NOTE to refer numbers in parenthesis to the IPL. All Models

601 Updated Part/Model Number address for Crimping Tool. All Models

602 Updated specification of conformal coating to Type UR. Updated nomenclature, All Models
specification, and manufacturer data of Primer PR-104 and PR-124.

603, 604 Deleted Surface Treatment Procedure. Added Battery Restoration Procedure to All Models
comply with TIL 384B.

605 Updated nomenclature of Primer in text. All Models

606-613 Text rolled. All Models

614 Updated figure number to 604 and 605. All Models

615 Text rolled. All Models

33-50-42 Highlights Page 1

Feb 1/06
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

Page No. Description of Change Effectivity

616 Updated figure number to 604 and 605. All Models

617 Text rolled. All Models

618 Updated figure number to 604 and 605. All Models

619 Updated Grimes Aerospace Co. phone number. Added steps to replace labels. All Models

620 Text rolled. All Models

702 Moved step for installation of instruction plate to Repair section. All Models

901 Changed Part/Model Number for Variable Regulated Power Supplies to All Models
Commercially Available.

1004 Updated Grimes Aerospace Co. phone number. All Models

1009, 1011 Updated Numerical Index with new label numbers. All Models

1012 Updated IPL Figure 1 to show new labels. All Models

1013 Added Superseded By data for items 5 and 10 and updated UPA for item 5. All Models

1015 Updated Detailed Parts Listing with new label data. All Models

33-50-42 Highlights Page 2

Feb 1/06
 GRIMES AEROSPACE COMPANY
A WHOLLY OWNED SUBSIDIARY OF HONEYWELL INTERNATIONAL
550 STATE ROUTE 55
URBANA, OHIO 43078

COMPONENT MAINTENANCE MANUAL

WITH
ILLUSTRATED PARTS LIST

EMERGENCY EXIT LIGHT POWER SUPPLY

PART NUMBERS

60-1321-1 60-1321-1LB
60-1321-5 60-1321-5LB
60-1321-7 60-1321-7LB

This document and all information and expression

contained herein are the property of Grimes Aerospace, are
loaned in confidence, and may not, in whole or in part, be
used, duplicated, or disclosed for any purpose without
prior written permission of Grimes Aerospace. All rights
reserved.

33-50-42 Page T-1

Feb 1/06
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

RECORD OF REVISIONS

Retain this record in the front of the manual. On receipt of revisions, insert revised pages in manual. Enter
revision number, date issued, date inserted and initials.

REV. DATE DATE REV. DATE DATE

NO. ISSUED INSERTED BY NO. ISSUED INSERTED BY

BASIC 3/1/83

1 6/30/93

2 7/1/00

3 10/1/05

4 2/1/06

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Feb 1/06
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

RECORD OF TEMPORARY REVISIONS

REV. ISSUE DATE DATE REV. ISSUE DATE DATE

NO. DATE INSRTD BY REMVD BY NO. DATE INSRTD BY REMVD BY

33-50-42 Page RTR-1/RTR-2

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

SERVICE BULLETIN LIST

SERVICE BULLETIN REVISION DATE BULLETIN

NUMBER NUMBER INCORPORATED INTO MANUAL

B5-21119 1 6/30/93

60-1321-33-0028 1 6/30/93

TIL 162 2 7/1/00

TIL 232A 2 7/1/00

TIL 177 2 7/1/00

TIL 327 2 7/1/00

TIL 82 2 7/1/00

TIL 384B 4 2/1/06

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

LIST OF EFFECTIVE PAGES

SUBJECT PAGE DATE SUBJECT PAGE DATE

Title Page T-1 Feb 1/06 Repair 601 Feb 1/06

Record of Revisions RR-1 Feb 1/06 602 Feb 1/06
RR-2 Blank 603 Feb 1/06
Record of Temporary RTR-1 Jul 1/00 604 Feb 1/06
Revisions RTR-2 Blank 605 Feb 1/06
Service Bulletin List SBL-1 Feb 1/06 606 Feb 1/06
SBL-2 Blank 607 Feb 1/06
List of Effective LEP-1 Feb 1/06 608 Feb 1/06
Pages LEP-2 Feb 1/06 609 Feb 1/06
Table of Contents TC-1 Jul 1/00 610 Feb 1/06
TC-2 Blank 611 Feb 1/06
Introduction INT-1 Jul 1/00 612 Feb 1/06
INT-2 Blank 613 Feb 1/06
Description and 1 Feb 1/06 614 Feb 1/06
Operation 2 Jul 1/00 615 Feb 1/06
3 Jul 1/00 616 Feb 1/06
4 Jul 1/00 617 Feb 1/06
5 Oct 1/05 618 Feb 1/06
6 Oct 1/05 619 Feb 1/06
7 Oct 1/05 620 Feb 1/06
8 Jul 1/00 Assembly (Including 701 Oct 1/05
Testing and 101 Feb 1/06 Storage) 702 Feb 1/06
Fault Isolation 102 Jul 1/00 703 Jul 1/00
103 Jul 1/00 704 Jul 1/00
104 Jul 1/00 Special Tools, Fixtures 901 Feb 1/06
105 Jul 1/00 and Equipment 902 Oct 1/05
106 Jul 1/00 903 Oct 1/05
107 Jul 1/00 904 Blank
108 Blank Illustrated Parts List 1001 Jul 1/00
Disassembly 301 Feb 1/06 1002 Jul 1/00
302 Jul 1/00 1003 Jul 1/00
Cleaning 401 Feb 1/06 1004 Feb 1/06
402 Blank 1005 Jul 1/00
Check 501 Oct 1/05 1006 Jul 1/00
502 Jul 1/00 1007 Jul 1/00
1008 Jul 1/00

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

SUBJECT PAGE DATE SUBJECT PAGE DATE

Illustrated Parts List, 1009 Feb 1/06
cont. 1010 Jul 1/00
1011 Feb 1/06
1012 Feb 1/06
1013 Feb 1/06
1014 Jul 1/00
1015 Feb 1/06
1016 Jul 1/00
1017 Jul 1/00
1018 Jul 1/00
1019 Jul 1/00
1020 Oct 1/05
1021 Jul 1/00
1022 Jul 1/00
1023 Jul 1/00
1024 Jul 1/00
1025 Jul 1/00
1026 Blank

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

TABLE OF CONTENTS

SUBJECT PAGE

Introduction ................................................................................................................................................. INT-1

Description and Operation ................................................................................................................................. 1

Testing and Fault Isolation ............................................................................................................................. 101

Automatic Test Requirements (ATLAS) ....................................................................................... Not Applicable

Disassembly ................................................................................................................................................... 301

Cleaning ......................................................................................................................................................... 401

Check ............................................................................................................................................................. 501

Repair ............................................................................................................................................................. 601

Assembly (Including Storage) ........................................................................................................................ 701

Fits and Clearances ..................................................................................................................... Not Applicable

Special Tools, Fixtures and Equipment ......................................................................................................... 901

Illustrated Parts List ..................................................................................................................................... 1001

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

INTRODUCTION

This publication contains shop maintenance instructions with Illustrated Parts List (IPL) for the emergency exit
light power supply, P/Ns 60-1321-1, -1LB, -5, -5LB, -7 and -7LB, manufactured by Grimes Aerospace
Company and hereafter referred to as the power supply.

The instructions in this publication provide information necessary to perform maintenance functions ranging
from simple checks and replacement to complete shop-type repair.

The instructions only apply to the power supply part numbers listed above. Be sure the part number on the
power supply is listed on the title page before performing any of these instructions.

This publication is written to the Air Transportation Association of America (ATA) Specification Number 100
and will be revised as necessary to show current information.

This publication is divided into sections as shown in the preceding Table of Contents. Also refer to the Table
of Contents for page location of each applicable section.

An explanation of how to use the Illustrated Parts List (IPL) is provided in the introduction of that section.

The following sections of this publication have been verified on the date(s) specified. Where actual
performance of the functions (tasks) cannot be performed prior to issuing a manual, those functions (tasks)
shall be verified by simulation. Any function (task) verified by simulation must be verified by actual
performance at the earliest possible time.

VERIFIED SECTION VERIFICATION DATE

Testing and Fault Isolation Verified by performance: April 20, 2000

Disassembly Verified by performance: April 20, 2000
Assembly Verified by performance: April 20, 2000

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

DESCRIPTION AND OPERATION

1. Description. (See Figure 1)

A. The power supply automatically energizes an external emergency exit light when aircraft power
failure occurs. An external switch controls the operation of the power supply. On power supply
P/N 60-1321-7, an external flight attendant switch can be used to operate the power supply.

B. Refer to Table 1 for power supply model data.

NOTE: Batteries are not provided on power supplies with an LB suffix in their part numbers.
In this manual, power supplies are assumed to have battery assemblies.

C. The power supply has three primary components:

• Cover assembly

• Battery assembly

• Housing assembly

D. The cover assembly allows access to the rechargeable battery assembly. The cover assembly
attaches to the housing assembly with quarter-turn fasteners for easy removal.

Power Supply
Figure 1

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COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

E. The battery assembly attaches to the cover assembly with quarter-turn fasteners. A support
assembly holds the housing assemblies and battery assembly together. It also has an insulator
assembly. The insulator assembly electrically connects the battery assembly and housing assembly.
The battery assembly has six C-size, nickel-cadmium cells welded together with nickel straps. A
fully charged battery assembly can energize an external emergency exit light for approximately 20
minutes.

F. The housing assembly contains the electrical components of the power supply. A connector on the
housing assembly connects the power supply to external control switches, emergency exit lights
and power sources. The housing assembly also has a terminal assembly to connect power to the
battery assembly.

Table 1. Power Supply Models

INPUT POWER BATTERY FLIGHT ATTENDANT

PART NUMBER
CHARGE ARM/DISARM ASSEMBLY SWITCH

60-1321-1 28 Vdc 28 Vdc Yes No

60-1321-1LB 28 Vdc 28 Vdc No No
60-1321-5 28 Vdc 28 Vdc Yes No
60-1321-5LB 28 Vdc 28 Vdc No No
60-1321-7 115 Vac 28 Vdc Yes Yes
60-1321-7LB 115 Vac 28 Vdc No Yes

2. Operation. (See Figure 2)

A. The power supply has components to prevent damage by voltage spikes. It also has components to
prevent power fluctuations from causing the power supply to operate incorrectly.

B. An external pilot’s switch controls the operation of the power supply. The power supply circuits
operate as follows:

(1) With the pilot’s switch in the ON position, the power supply operates as it does during a power
failure. The pilot’s switch can be set to ON to test the power supply.

(2) With the pilot’s switch in the ARMED position, current on the input charge line charges the
battery assembly. If a power failure occurs, the power supply automatically energizes an exit
light.

(3) With the pilot’s switch in the OFF position, the silicon-controlled rectifier (SCR1) goes off. This
causes the power supply to go off. This is done after a power failure to prepare the power
supply for normal operation.

C. On power supply P/N 60-1321-7, a flight attendant’s switch is used to operate the power supply.
When set to ON, the power supply energizes the exit light.

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COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

D. Power supply ON function.

(1) With the pilot’s switch in the ON position, 28 Vdc is applied to the power supply ARM circuit
through connector (J1), pin 3. Power is removed from the CHARGE circuit on connector (J1),
pin 2.

(2) Power removed from connector (J1), pin 2, causes the junction of diode (CR7) and
resistors (R12 and R14) to go low. This applies a low to the inputs of integrated circuit (U1),
pins 1 and 2. The output of integrated circuit (U1), pin 3, goes high.

(3) The voltage on connector (J1), pin 3, is applied to the gate of silicon-controlled rectifier (SCR1).
This causes silicon-controlled rectifier (SCR1) to conduct. Battery current flows through silicon-
controlled rectifier (SCR1) and causes transistors (Q1 and Q2) to switch on.

(4) When transistors (Q1 and Q2) conduct, zener diode (CR4) applies regulated power (Vcc) to
integrated circuit (U1), pin 14. Current also flows through potentiometer (R15). This causes the
input of integrated circuit (U1), pin 9, to go high.

(5) With both inputs of integrated circuit (U1), pins 9 and 10, at a high level, the output of
integrated circuit (U1), pin 8, goes low. The inputs of integrated circuit (U1), pins 4 and 5, also
go low. The output of integrated circuit (U1), pin 6, then goes high.

(6) When the outputs of integrated circuit (U1), pins 3 and 6, both go high, transistor (Q3)
conducts. This causes transistors (Q4 and Q5) to switch on. Battery current flows through
transistor (Q5) and causes the emergency exit light to come ON.

E. Low voltage shutoff function.

(1) A circuit latches the power supply OFF when the battery voltage goes below a set shutoff level.
This causes the emergency exit light to go OFF. The latch circuit prevents battery damage
caused by cell reversal. This can occur when the battery cells discharge too much. The pilot’s
switch must be set to OFF and power must be applied to the input to release the latch circuit.

(2) Potentiometer (R15) sets the shutoff level. When the battery voltage drops to 5.2 to 5.6 Vdc,
potentiometer (R15) applies a low to integrated circuit (U1), pin 9.

(3) The output of integrated circuit (U1), pin 8, goes high. The inputs at integrated circuit (U1),
pins 4 and 5, also go high. This causes the output of integrated circuit (U1), pin 6, to go low.
This causes transistors (Q3, Q4 and Q5) to shut off. The emergency exit light goes OFF.

(4) Integrated circuit (U1) inverts the high signal at pin 8 at pins 12 and 13. The output of
integrated circuit (U1), pin 11, goes low. This latches the output of integrated circuit (U1), pin 8,
high. The circuit stays in this condition until the latch circuit is released.

F. Power supply ARMED function.

(1) With the pilot’s switch in the ARMED position, input power is applied to the power supply
through connector (J1), pins 2 and 3.

(2) On power supply P/N 60-1321-7, resistor (R20), capacitors (C6 and C7) and diodes (CR9
and CR10) make a half-wave rectifier. This circuit converts the 115-Vac input at connector (J1),
pin 2, to direct current. The rectifier circuit applies this dc voltage to blocking diode (CR1).

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COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

(3) Current flows through blocking diode (CR1), current limiting-resistor (R1) and battery
assembly (BT1) to ground at connector (J1), pin 5. Battery assembly (BT1) charges
continuously until a power failure occurs.

(4) Power removed from connector (J1), pin 2, causes the junction of diode (CR7) and
resistors (R12 and R14) to go low. This applies a low to the inputs of integrated circuit (U1),
pins 1 and 2. The output of integrated circuit (U1), pin 3, goes high.

(5) The voltage on connector (J1), pin 3, goes to the gate of silicon-controlled rectifier (SCR1). This
causes silicon-controlled rectifier (SCR1) to conduct. Battery current flows through silicon-
controlled rectifier (SCR1) and causes transistors (Q1 and Q2) to turn on.

(6) When transistors (Q1 and Q2) conduct, zener diode (CR4) applies regulated power (Vcc) to
integrated circuit (U1), pin 14. Current also flows through potentiometer (R15). This causes the
output of integrated circuit (U1), pin 9, to go high.

(7) With both inputs of integrated circuit (U1), pins 9 and 10, at a high level, the output of
integrated circuit (U1), pin 8, goes low. The inputs of integrated circuit (U1), pins 4 and 5, also
go low. The output of integrated circuit (U1), pin 6, then goes high.

(8) When the outputs of integrated circuit (U1), pins 3 and 6, both go high, transistor (Q3)
conducts. This causes transistors (Q4 and Q5) to switch on. Battery current flows through
transistor (Q5) and causes the emergency exit light to turn ON.

G. Power supply OFF function.

(1) With the pilot’s switch in the OFF position, input power is applied to connector (J1), pins 2
and 4.

(2) On power supply P/N 60-1321-7, resistor (R20), capacitors (C6 and C7) and diodes (CR9
and CR10) make a half-wave rectifier. This circuit converts the 115-Vac input at connector (J1),
pin 2, to direct current.

(3) Current flows through diode (CR6). This causes the junction of resistors (R12 and R14) and
diode (CR7) to go high. The potentials on both sides of diode (CR7) balance. The causes the
output of integrated circuit (U1), pin 3, to go low. Transistors (Q3, Q4 and Q5) switch off. This
stops the flow of current through transistor (Q5) and to the emergency exit light.

(4) The voltage from connector (J1), pin 4, back-biases silicon-controlled rectifier (SCR1). This
stops the flow of current from battery assembly (BT1) through silicon-controlled
rectifier (SCR1). Transistors (Q1 and Q2) switch off. This removes the regulated power (Vcc)
from integrated circuit (U1).

H. Flight attendant’s switch function (power supply P/N 60-1321-7 only).

(1) When the flight attendant’s switch is set to ON, ground potential is removed from the junctions
of diodes (CR11 and CR12). This allows current from the charge circuit to flow to the base of
transistor (Q6). This causes transistor (Q6) to conduct. This causes transistors (Q7 and Q5) to
switch on. Battery current flows through transistor (Q5) and causes the emergency exit light to
come ON.

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

Power Supply Schematic (Sheet 1 of 3)

Figure 2

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

Power Supply Schematic (Sheet 2 of 3)

Figure 2

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

Power Supply Schematic (Sheet 3 of 3)

Figure 2

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

(2) When the flight attendant’s switch is set to NORMAL, ground potential is applied to the
junctions of diodes (CR11 and CR12). This switches transistor (Q6) off. Transistors (Q7
and Q5) then switch off. This stops the flow of current through transistor (Q5) and to the
emergency exit light.

3. Leading Particulars. (Refer to Table 2)

Table 2. Leading Particulars

DESCRIPTION DATA

Dimensions:
Length ................................................................................................................... 8.75 inches (222,3 mm)
Width ..................................................................................................................... 5.50 inches (139,7 mm)
Height ..................................................................................................................... 2.66 inches (67,6 mm)
Weight (max): ................................................................................................................. 3.50 pounds (1,6 kg)
Electrical:
Input Voltage (charge circuit)
P/N 60-1321-1 ................................................................................................................. 25 to 28 Vdc
P/N 60-1321-5 ..................................................................................................................25 to 28 Vdc
P/N 60-1321-7 ........................................................................................................... 115 Vac, 400 Hz
Input Current Draw (charge) ............................................................................................... 255 to 275 mA
Input Voltage (ARM/DISARM circuits) ................................................................................... 18 to 31 Vdc
Charge Time @ 28 Vdc ................................................................................................................ 16 hours
Output Voltage (min) ...................................................................................................................... 6.4 Vdc
Output Current Draw (max) ......................................................................................................... 4.5 amps
Battery Discharge Time
At 68 °F (°C) ...................................................................................................................... 20 minutes
At 30 °F (°C) ...................................................................................................................... 10 minutes
Battery Shutoff Voltage (adjustable) .................................................................................... 5.4 to 5.8 Vdc

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

TESTING AND FAULT ISOLATION

1. General Information.

A. The following paragraphs provide information for testing and fault isolation of the power supply.

B. Conduct all tests at a temperature of 65 to 85 °F (18 to 29 °C) and in the order presented, unless
otherwise noted. Failure of any test is cause for failure of the power supply. Correct the fault before
testing is continued.

C. Refer to Table 101 for a list of special tools, fixtures and equipment needed for testing and fault
isolation. Refer to Table 102 for a list of materials needed for testing and fault isolation. Equivalent
substitutes are acceptable.

Table 101. Special Tools, Fixtures and Equipment List

NOMENCLATURE PART/MODEL USED FOR FIGURE

NUMBER NUMBER
Digital Multimeter Model 87 Testing and NA
(DMM) (0 to 200 V, Fluke Corp. Fault Isolation
0 to 2000 mA, Everett, WA (V89536)
Accuracy ±1%)
(Qty. 2)
Variable Regulated Commercially Available Testing and NA
Power Supply Fault Isolation
(0-45 Vdc, 6-amp min)
Variable Regulated Commercially Available Testing and NA
Power Supply Fault Isolation of P/N
(0-120 Vac, 400 Hz) 60-1321-7 only
Tester 71572 Testing and 901
Grimes Aerospace Co. Fault Isolation
Urbana, OH (V72914)
Tester 63845 Testing and 902
Grimes Aerospace Co. Fault Isolation
Urbana, OH (V72914)

Table 102. Materials List

NOMENCLATURE SPECIFICATION MANUFACTURER

Cleaning Cloth A-A-59323 Commercially Available
Adhesive (AD-195*) 1201 General Electric Co.
Semi-Conductor Products Dept.
Power Components Opn.
Auburn, NY (V09214)
*Grimes reference only.

2. Pretest Procedures.

A. Review any shipping tags or forms to determine cause for removal from aircraft.

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COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

B. Wipe the power supply with a clean cloth to remove dirt, dust and foreign material.

C. Visually inspect the power supply for signs of missing, broken, bent or cracked parts. Damaged
parts shall be replaced before the power supply is tested.

3. Test Setup. (See Figure 101)

NOTE: Refer to IPL Figure 1 for an illustration. Numbers in parentheses ( ) refer to item
numbers on the illustration.

Power supply P/N 60-1321-7 must be tested with tester 63845.

Power supply P/N 60-1321-7 uses an AC and a DC power supply for following test.

Power supply P/Ns 60-1321-1 and -5 use only a DC power supply for following test.

Use a fully charged battery assembly.

After 16 hours of continuous charging at room temperature and at 25 to 28 volts, the

power supply shall supply a load of 4.1 amps with a minimum output terminal voltage
of 6.4 volts for 20 minutes at room temperature or 10 minutes at 30 °F (-1 °C).

A. Ensure power supplies are set to zero volts and are OFF.

B. Loosen four studs (20) and remove cover subassembly (-15) and battery assembly (-115A) from
power supply under test.

C. Position cover subassembly (-15) on power supply under test and tighten four studs (20).

D. Connect power supply under test to test setup.

E. Set DMM #1 to read 200 Vdc.

F. Set DMM #2 to read 2000 mA DC.

G. If using tester P/N 71572, set tester switches as follows:

(1) Set switch S1 to OFF.

(2) Set switch S2 to NORMAL.

(3) Set switch S5 to OFF.

(4) Set dropout control rheostat fully clockwise.

H. If using tester P/N 63845, set tester switches as follows:

(1) Set switch S1 to OFF.

(2) Set switch S2 to NORMAL.

(3) Set switch S5 to OFF.

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COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

(4) Set dropout control rheostat fully clockwise.

(5) If testing power supply P/N 60-1321-7, set switch S9 to 115. If testing power supply
P/Ns 60-1321-1 or 60-1321-5, set switch S9 to 28.

Test Setup
Figure 101

4. Testing.

NOTE: Refer to the IPL for illustrations. Numbers in parentheses ( ) refer to item numbers on the
illustration.

A. Turn on DC power supply and adjust it to 28 ±0.4 Vdc.

B. If testing power supply P/N 60-1321-7, turn on AC power supply and adjust it to 115 ±0.1 Vac.

C. Note reading of DMM #1.

• Minimum voltage shall be 7.8 Vdc.

D. Set switch S1 on tester to ARM.

E. If testing power supply P/Ns 60-1321-1 and -3, momentarily depress switch S6 on tester.

• Load lamps on tester shall illuminate.

F. If testing power supply P/N 60-1321-7, momentarily turn AC power supply OFF.

• Load lamps on tester shall illuminate.

G. Set switch S1 on tester to ON and note reading of DMM #1.

• Load lamps on tester shall illuminate.

• Initial minimum voltage shall be 7.2 Vdc.

H. Set switch S1 on tester to ARM.

• Load lamps on tester shall extinguish.

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PART NUMBER 60-1321

I. Momentarily depress switch S4 on tester and note reading of DMM #2.

• Current reading shall be 160 ±25 mA.

J. Set switch S2 on tester to DROPOUT.

K. Set switch S1 on tester to ON.

• Load lamps on tester shall illuminate.

L. Depress switch S3 on tester and slowly rotate DROPOUT CONTROL rheostat counterclockwise.
Observe reading on DMM #1 as load lamps on tester extinguish. Adjust potentiometer (R15) (70,
IPL Figure 3) to obtain required reading on DMM.

• Voltage reading shall be 5.6 ±0.2 Vdc as load lamps on tester extinguish.

M. Release switch S3 on tester.

N. Set switch S2 on tester to NORMAL.

O. Set switch S1 on tester to OFF.

P. Depress switch S4 on tester and observe reading on DMM #2.

• Current reading shall be 255 ±30 mA.

Q. Set switch S1 on tester to ARM and then to ON.

• Load lamps on tester shall illuminate.

R. Set switch S1 on tester to OFF.

• Load lamps on tester shall extinguish.

S. If testing power supply P/N 60-1321-5, momentarily depress switch S8 on tester.

• CHG CKT DIODE IND lamp on tester shall illuminate.

T. If testing power supply P/N 60-1321-7, momentarily depress switch S7 on tester.

• Load lamps on tester shall illuminate while switch S7 on tester is depressed.

U. Turn dc power supply OFF.

V. Turn ac power supply OFF (if applicable).

W. Loosen four studs (20, IPL Figure 1) and remove cover subassembly (-15) from power supply under
test.

X. Install battery assembly (-115A) in power supply under test.

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PART NUMBER 60-1321

Y. Position cover subassembly (-15) on power supply under test and tighten four studs (20).

• Load lamps on tester shall remain extinguished.

Z. Turn dc power supply ON.

AA. Turn ac power supply ON (if applicable).

BB. Repeats steps Q. and R.

CC. Turn power supplies OFF and disconnect power supply under test from test setup.

DD. Loosen four studs (20) and remove cover subassembly (-15) from power supply under test.

WARNING: ADHESIVE IS HIGHLY FLAMMABLE. AVOID INHALATION OF VAPORS AND

CONTACT WITH SKIN. OBSERVE FIRE PRECAUTIONS.

EE. Seal adjustment screw of potentiometer (R15) (70, IPL Figure 3) with adhesive. Use a clean cloth to
remove excess adhesive. Allow to air dry for 4 hours.

FF. Position cover subassembly (-15, IPL Figure 1) on power supply under test and tighten four
studs (20).

5. Posttest Procedures.

A. If power supply passed all the tests, prepare it for shipment or storage. Refer to ASSEMBLY,
section 701, for details.

B. If power supply did not pass all the tests, repair or replace defective parts, then repeat all tests.
Refer to Fault Isolation, paragraph 6, for details.

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COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

6. Fault Isolation. (Refer to Table 103)

NOTE: Refer to the IPL for illustrations. Numbers in parentheses ( ) refer to item numbers on the
illustration.

Table 103. Fault Isolation (Sheet 1 of 2)

FAULT PROBABLE CAUSE CORRECTIVE ACTION

Battery assembly (-115A, IPL 1. Defective battery assembly 1. Recharge or replace battery
Figure 1) does not accept correct (-115A). assembly (-115A).
charge.
2. Defective diode (CR1) (175, 2. Replace diode (CR1) (175).
IPL Figure 3).
3. Defective resistor (R1) (5, IPL 3. Replace resistor (R1) (5).
Figure 2).
Battery assembly (-115A, IPL Defective battery assembly Replace battery assembly
Figure 1) loads down to less than (-115A). (-115A).
7.2 volts during battery test (see
step 4.G.).
Load lamps on tester do not 1. Defective transistors (Q4) (125, 1. Apply ground potential to
illuminate when switch S1 on IPL Figure 3) and (Q5) (75). junction of transistor (Q4)
tester is set to ARM (see steps (125) and resistor (R13)
4.G. and 4.K.). (140). If load lamps on tester
do not illuminate, replace
transistor (Q5) (75). If load
lamps on tester illuminate,
replace transistor (Q4) (125).
2. Defective transistors (Q1 and 2. Use a digital multimeter
Q3) (145), (Q2) (60) and (DMM) to measure back-to-
(Q4) (125). back ratio of transistors (Q1
and Q3) (145), (Q2) (60) and
(Q4) (125). Replace defective
transistors (Q1 and Q3) (145),
(Q2) (60) and (Q4) (125).
3. Defective diodes (CR1) (175) 3. Use a DMM to measure back-
and (CR2, CR3, CR6 and to-back ratio of diodes (CR1)
CR7) (5). (175) and (CR2, CR3, CR6
and CR7) (5). Replace
defective diodes (175), (CR2,
CR3, CR6 and CR7) (5).
4. Defective rectifier (SCR1) (15). 4. Replace defective rectifier
(SCR1) (15).
5. Defective integrated circuit 5. Replace integrated circuit
(U1) (160). (U1) (160).

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

Table 103. Fault Isolation (Sheet 2 of 2)

FAULT PROBABLE CAUSE CORRECTIVE ACTION

Load lamps on tester do not Defective capacitors (C2) (35) Replace defective capacitors
illuminate when power is and (C5) (50). (C2) (35) and (C5) (50).
removed during battery test (see
step 4.BB.).
Load lamps on tester do not Defective diode (CR5) (5). Replace defective diode
extinguish when switch S1 on (CR5) (5).
tester is set to OFF.
Load lamps on tester do not 1. Potentiometer (R15) (70) not 1. Adjust potentiometer (R15)
extinguish at correct low voltage adjusted correctly. (70). Refer to step 4.L. and
shutoff level (see step 4.L.). adjust potentiometer (R15)
(70) to a low-voltage shutoff
level of 5.6 ±0.2 Vdc.
2. Defective potentiometer (R15) 2. Replace potentiometer (R15)
(70). (70).
3. Defective integrated circuit (U1) 3. Replace integrated circuit
(160). (U1) (160).
Load lamps on tester do not 1. Defective transistor (Q6) (15, 1. Replace transistor (Q6) (15).
illuminate when switch S7 on IPL Figure 4).
tester is depressed (see
step 4.T.). 2. Defective diode (CR12) (40). 2. Replace diode (CR12) (40).

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

DISASSEMBLY

1. General Information.

A. The following paragraphs provide information for disassembly of the power supply.

B. Disassemble only to the extent required to replace defective parts, unless complete overhaul is
required. Before disassembly, wipe exterior surfaces with a clean cloth to remove dust, dirt or other
foreign materials.

C. Do not remove threaded inserts. Refer to CHECK, section 501, for details.

D. Do not disassemble riveted parts. Refer to REPAIR, section 601, to determine whether part(s) can
be replaced.

E. Do not remove electrical wires unless repair or replacement is required. Tag electrical wires before
removal.

F. Refer to Table 301 for a list of materials needed for disassembly. Equivalent substitutes are
acceptable.

Table 301. Materials List

NOMENCLATURE SPECIFICATION MANUFACTURER

Cleaning Cloth A-A-59323 Commercially Available

2. Disassembly of Power Supply.

NOTE: Refer to IPL Figure 1 for an illustration. Numbers in parentheses ( ) refer to item numbers
on the illustration.

A. Loosen four studs (20) and remove cover subassembly (-15) and battery assembly (-115A) from
housing subassembly (300).

B. Loosen studs (155) and (160) and separate battery assembly (-115A) from cover
subassembly (-15).

3. Disassembly of Battery Assembly.

NOTE: Refer to IPL Figure 1 for an illustration. Numbers in parentheses ( ) refer to item numbers on
the illustration.

A. Remove four screws (125) and separate support (165) from battery assembly (-115A); take care not
to damage wires leading to battery assembly (-115A).

B. Remove three washers (150), stud (155) and two studs (160) from support (165).

C. Remove stopnut (145), washer (140), insulator (130) and screw (135) from support (165); take care
not to damage wires leading to battery assembly (-115A).

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PART NUMBER 60-1321

D. Remove six screws (175), housing (185), two cushioning pads (190) and battery assembly
(BT1) (275) from housing (295).

4. Disassembly of Cover Assembly.

NOTE: Refer to IPL Figure 1 for an illustration. Numbers in parentheses ( ) refer to item numbers on
the illustration.

A. Remove four studs (20) and washers (25) from cover plate (110).

B. Remove two locknuts (45) and receptacles (40) from bracket subassemblies (-50).

C. Remove four screws (35) and two bracket subassemblies (-50) from cover plate (110).

D. Remove two screws (70) and bracket assembly (-65) from cover plate (110).

E. Remove six screws (175), housing (185), two cushioning pads (190) and battery assembly
(BT1) (275) from housing (295).

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

CLEANING

1. General Information.

A. The following paragraphs provide information for cleaning the power supply.

B. Refer to Table 401 for a list of materials needed for cleaning. Equivalent substitutes are acceptable.

Table 401. Materials List

NOMENCLATURE SPECIFICATION MANUFACTURER

Aqueous Cleaner Armakleen M-HP II Safety-Kleen Systems, Inc.
Columbia, SC (V30530)
Cleaning Cloth A-A-59323 Commercially Available
Soft, Natural Bristle Brush None Commercially Available

2. Cleaning Procedures.

NOTE: Refer to IPL Figure 1 for an illustration. Numbers in parenthesis ( ) refer to item numbers
on the illustration.

A. Clean metal parts in aqueous cleaner. Use a soft, natural, bristle brush to remove ground-in
deposits.

B. Use a clean cloth dampened with aqueous cleaner to remove old adhesive/sealant residue from
parts.

C. Except for printed circuit boards, wipe electrical parts with a clean cloth dipped in aqueous cleaner
to remove dirt, dust, and foreign material.

D. Wipe printed circuit boards with a dry, clean cloth to remove dirt or dust.

WARNING: AIR PRESSURE SHALL BE LIMITED TO 30 PSI (207 KPA). FAILURE TO COMPLY
MAY RESULT IN INJURY OR DEATH TO PERSONNEL.

E. Dry parts with compressed air or wipe with a clean cloth and allow to air-dry.

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

CHECK

1. General Information.

A. The following paragraphs provide information for a check of each part in the power supply.

B. Complete checks in accordance with the standard requirements and checks listed in the following
paragraphs, unless otherwise specified.

C. Refer to Table 501 for a list of materials needed for checks. Equivalent substitutes are acceptable.

Table 501. Materials List

NOMENCLATURE SPECIFICATION MANUFACTURER

Cleaning Cloth A-A-59323 Commercially Available

2. Standard Requirements.

A. Clean the parts before performing any check. Refer to CLEANING, section 401, for details.

B. Use 2X magnification and an amplified light to check the parts.

C. Repair or replace the parts that exceed limits. Refer to REPAIR, section 601, for details. Use parts
within limits for assembly. Refer to ASSEMBLY, section 701, for details.

3. Standard Checks.

A. Examine parts for nicks, gouges, scratches or small burrs. If any are deeper than 0.03 inch
(0,76 mm), replace part. Minor damage may be repaired.

B. Examine parts for corrosion. If deeper than 0.03 inch (0,76 mm) or more than 20 percent of surface
is damaged, replace part. Minor damage may be repaired.

C. Examine painted parts for scratches, peeling, flaking or chipping. Minor damage may be repaired.
See REPAIR, section 601, for details.

D. Examine threaded parts with a thread gage for distortion or stripping. If not a Class-3 fit, replace
part.

E. Examine threaded inserts for stripping and tight fit. If damaged or loose, replace part.

F. Examine electrical parts for cracks, distortion, bent pins or signs of burned connections. If damaged,
replace parts.

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COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

4. Checks on Power Supply. (Refer to Table 502)

NOTE: Refer to the IPL for illustrations. Numbers in parentheses ( ) refer to item numbers on the
illustration.

Table 502. Checks on Power Supply

CHECK FOR ACTION

Studs (20, 155 and 160, IPL Figure 1), Washers (25) and (150) and Bracket Subassembly (-50)
Missing or damaged. Replace damaged studs (20, 155 and 160), washers (25 and 150) or bracket
subassembly (-50).
Insulator (130)
Damaged or corroded Clean contacts or replace insulator (130).
contacts.
Battery Assembly (-115A)
Corrosion or leakage. Clean or replace battery assembly (-115A).
Electrical Wiring
Cracks, breaks or Replace electrical wiring.
deterioration of insulation.
Printed Circuit Card Assembly (20, IPL Figure 2)
1. Damaged compo- 1. Replace damaged components.
nents.
2. Damaged traces or 2. Replace printed circuit card assembly (20).
pads.
Circuit Card Assembly (140)
1. Damaged compo- 1. Replace damaged components.
nents.
2. Damaged traces or 2. Replace printed circuit card assembly (140).
pads.
Terminal Assembly (-85)
1. Corrosion. 1. Clean terminal assembly (-85).
2. Damaged termi- 2. Replace terminals (105) or banana plugs (110).
nals (105) or banana
plugs (110).
Connector (J1) (45)
Missing or damaged Replace contacts and seal plugs.
contacts and seal plugs.

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

REPAIR

1. General Information.

A. The following paragraphs provide information for repair of parts in the power supply.

B. Limit repair procedures to correction of minor defects or damage, paint touch-up and replacement of
parts. Refer to CHECK, section 501, for details.

CAUTION: HEAT-SENSITIVE PARTS. USE A HEAT SINK; APPLY HEAT FOR A MAXIMUM OF
10 SECONDS AT A TEMPERATURE NOT TO EXCEED 300 °F (149 °C) TO AVOID
DAMAGE.

C. Apply solder in accordance with MIL-STD-454. Remove excess with a clean cloth.

WARNING: CONFORMAL COATING IS FLAMMABLE AND TOXIC TO EYES, SKIN AND

RESPIRATORY TRACT. SKIN AND EYE PROTECTION REQUIRED. AVOID
REPEATED OR PROLONGED CONTACT. USE ONLY IN WELL-VENTILATED
AREAS. KEEP AWAY FROM OPEN FLAMES OR OTHER SOURCES OF
IGNITION.

D. Use conformal coating to seal solder connections and electronic parts in accordance with
MIL-STD-275.

E. Use same color and type to replace electrical wires. Strip insulation 0.25 inch (6,35 mm). Use solder
to tin end, then attach to another component.

F. Install rivets in accordance with MIL-R-47196.

CAUTION: DO NOT USE CROCUS CLOTH ON ALUMINUM PARTS. CLOTH CONTAINS IRON
OXIDE, WHICH CAUSES RAPID OXIDATION OF ALUMINUM.

G. Use aluminum oxide abrasive cloth on aluminum parts. Use crocus cloth on steel parts.

H. Refer to Table 601 for a list of special tools, fixtures and equipment required for repair. Refer to
Table 602 for a list of materials needed for repair. Equivalent substitutes are acceptable.

Table 601. Special Tools, Fixtures and Equipment List

NOMENCLATURE PART/MODEL USED FOR FIGURE

NUMBER NUMBER
Arbor Press Drake Model 3A Repair NA
MSC Industrial
Supply Co.
Jonestown, PA (V08NV1)
Soldering Iron Commercially Available Repair NA
Crimping Tool M22520/1-01 Repair NA
Crimping Tool 47386 Repair NA
Tyco Electronics Corp.
Middletown, PA (V00779)
Extraction/Insertion Tool TH554 FT8 Electrical Contact NA
Daniels Mfg. Corp. Replacement
Orlando, FL (V11851)
Heat Gun Commercially Available Heat Shrink Tubing NA

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

Table 602. Materials List (Sheet 1 of 2)

NOMENCLATURE SPECIFICATION MANUFACTURER

Aluminum Oxide Abrasive Cloth P-C-451 (400-Grade) Commercially Available
Cleaning Cloth A-A-59323 Commercially Available
Conformal Coating (CM238*) MIL-I-46058, Type UR Commercially Available
Crocus Cloth P-C-458 (600-Grade) Commercially Available
Primer (PR-124*) MIL-C-8514 Commercially Available
Primer (PR-184*) BMS 10-11 Epoxy Deft, Inc.
(Green) Irvine, CA (V33461)
Paint (PA-404*) P6094 Vanguard Paint and Finishes, Inc.
Marietta, OH (V63717)
Adhesive (AD-040*) 102 General Electric Co.
Semi-Conductor Products Dept.
Power Components Opn.
Auburn, NY (V09214)
Primer (AD-059*) 1200 Dow Corning Corp.
Midland, MI (V71984)
Adhesive (AD-053*) 738 Dow Corning Corp.
Midland, MI (V71984)
Terminal (TE-089*) 36151 Amp, Inc.
(Qty. 2) (Supersedes P/N 31882) Middletown, PA (V00779)
Contact M39029/31-241 Commercially Available
(Qty. 12)
Seal Plug MS27488-20 Commercially Available
(Qty. 3)
Heat Shrink Tubing M23053-5-104-0 Commercially Available
(1.5 inches [38 mm])
Heat Shrink Tubing (TU-285*) HS101-1/8 Insultab, Inc.
(2 inches [51 mm]) Woburn, MA (V12509)
Tubing (TU-170*) INSUL TFE 300 Insultab, Inc.
(2 inches [51 mm]) Woburn, MA (V12509)
Wire (WI-954*) 1/8-inch nominal flat width, Nesor Alloy Corp.
(7 inches [178 mm]) Braided, tinned cadmium-copper, West Caldwell, NJ
160/0.0031 stranding (V5R551)
Wire (WI-348*) MIL-W-16878/4 Commercially Available
(3 inches [76 mm])
Wire (WI-502*) MIL-W-16878/4 Commercially Available
(140.625 inches [3571,88 mm])
*Grimes reference only.

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

Table 602. Materials List (Sheet 2 of 2)

NOMENCLATURE SPECIFICATION MANUFACTURER

Bus Wire (WI-646*) QQ-W-343 Type S Commercially Available
(2.5 inches [64 mm])
Wire (WI-421*) MIL-W-16878/4 Commercially Available
(20 inches [508 mm])
Wire (WI-438*) MIL-W-16878/4 Commercially Available
(17 inches [432 mm])
Wire (WI-490*) MIL-W-16878/4 Commercially Available
(2 inches [51 mm])
Wire (WI-520*) MIL-W-16878/4 Commercially Available
(6 inches [152 mm])
Wire (WI-552*) MIL-W-16878/4 Commercially Available
(5 inches [127 mm])
Wire (WI-562*) MIL-W-16878/4 Commercially Available
(5.5 inches [140 mm])
Electrical Solder SN63 WRMAP-3 Commercially Available
Masking Tape 0.75-Inch Wide Commercially Available
*Grimes reference only.

2. Battery Restoration Procedure

A. Discharge (See Figure 601)

(1) Discharge each cell in the battery assembly (BT1) (275, IPL Figure 1) separately until the
voltage across each cell is below 0.2 Vdc. Immediately remove the load.

Battery Discharge Setup

Figure 601

B. Charge (See Figure 602)

(1) Charge the battery assembly (BT1) (275, IPL Figure 1) with 250 - 275 mA initially for at least 16
hours.

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PART NUMBER 60-1321

NOTE: More than one battery pack can be charged at the same time when the
battery packs are connected in series. Battery packs should not be
charged in parallel without individual charging resistors. For example,
use a 28-Vdc power supply and a 75-ohm/5W resistor to charge each
battery (six series-connected cells).

Battery Pack Charge Setup

Figure 602

C. Capacitance Test (See Figure 603)

CAUTION: DISCHARGE OF THE BATTERY PACK DURING THIS TEST FOR MORE THAN 20
MINUTES CAN CAUSE DAMAGE OF ONE OR MORE CELLS BECAUSE OF CELL
REVERSAL.

(1) Connect the battery assembly (BT1) (275, IPL Figure 1) to a 2-ohm, 50W adjustable resistor
set for 1.72 to 1.76 ohms; e.g., Ohmite D50K2R0 through an ammeter. The battery pack must
deliver 3.75 Amps, minimum, for 20 minutes. During discharge, the minimum cell voltage must
be 1.1 Vdc. If the cell voltage is less than 1.1 Vdc, replace the cell.

Battery Cell Capacitance Test Setup

Figure 603

D. Charge

(1) Recharge the battery assembly (BT1) (275) after the capacitance test. Refer to step B.

3. Standard Repair Procedures

CAUTION: DO NOT CHANGE SURFACE FINISH OR PART SHAPE OR EXCEED WEAR LIMITS.
FAILURE TO COMPLY CAN RESULT IN FAILURE OF THE PART.

A. Remove minor surface corrosion with correct abrasive cloth.

B. Remove nicks, gouges, scratches or small burrs as follows:

(1) Remove any raised material with a very fine file.

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PART NUMBER 60-1321

(2) Blend damaged area into adjacent surfaces.

(3) Polish areas with correct abrasive cloth.

4. Surface Finish Procedure. This procedure shall be used for touch-up of scratches and surface defects.

NOTE: Refer to the IPL for illustrations. Numbers in parentheses ( ) refer to item numbers on the
illustration.

A. Repair area if required. Refer to Standard Repair Procedures, paragraph 2, for details.

B. Apply chemical film to surface if required. Refer to Surface Treatment Procedure, paragraph 3, for
details.

C. If not already done, cover areas not to be treated with masking tape.

WARNING: PRIMER IS FLAMMABLE AND TOXIC TO EYES, SKIN AND RESPIRATORY

TRACT. SKIN AND EYE PROTECTION REQUIRED. AVOID REPEATED OR
PROLONGED CONTACT. USE ONLY IN WELL-VENTILATED AREAS. KEEP
AWAY FROM OPEN FLAMES OR OTHER SOURCES OF IGNITION.

D. Apply primer (PR-124) to exterior surfaces of housing (160, IPL Figure 2) and cover plate (110, IPL
Figure 1) as follows:

(1) Mix and thin primer in accordance with manufacturer’s instructions.

(2) Apply one coat of primer to damaged area. Allow to air dry or place in an oven for one hour at
200 °F (93 °C).

(3) When dry, check finish is smooth and free of defects.

WARNING: PRIMER IS FLAMMABLE AND TOXIC TO EYES, SKIN AND RESPIRATORY

TRACT. SKIN AND EYE PROTECTION REQUIRED. AVOID REPEATED OR
PROLONGED CONTACT. USE ONLY IN WELL-VENTILATED AREAS. KEEP
AWAY FROM OPEN FLAMES OR OTHER SOURCES OF IGNITION.

E. Apply primer (PR-184) to exterior surfaces of housing (160, IPL Figure 2) and cover plate (110, IPL
Figure 1) as follows:

(1) Mix and thin primer in accordance with manufacturer’s instructions.

(2) Apply one coat of primer to damaged area. Allow to air dry or place in an oven for one hour at
200 °F (93 °C).

(3) When dry, check finish is smooth and free of defects.

WARNING: PAINT IS FLAMMABLE AND TOXIC TO EYES, SKIN AND RESPIRATORY TRACT.
SKIN AND EYE PROTECTION REQUIRED. AVOID REPEATED OR PROLONGED
CONTACT. USE ONLY IN WELL-VENTILATED AREAS. KEEP AWAY FROM OPEN
FLAMES OR OTHER SOURCES OF IGNITION.

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PART NUMBER 60-1321

F. Apply paint to exterior surfaces of housing (160, IPL Figure 2) and cover plate (110, IPL Figure 1) as
follows:

(1) Mix and thin paint in accordance with manufacturer’s instructions.

(2) Apply one coat of paint to damaged area. Allow to air dry or place in an oven for one hour at
200 °F (93 °C).

(3) When dry, apply a second coat of paint. Allow to air dry or place in an oven for one hour at
200 °F (93 °C).

(4) When dry, remove masking tape and check finish is smooth, free of defects and blends into
other surfaces.

5. Repair of Cover Subassembly.

NOTE: Refer to IPL Figure 1 for an illustration. Numbers in parentheses ( ) refer to item numbers
on the illustration.

A. Replace handle (95) as follows:

(1) Drill out four rivets (100) and remove two plates (105) and handle (95) from cover plate (110).
Discard handle (95).

(2) Position new handle (95) and two plates (105) on cover plate (110) and align holes.

(3) Install four new rivets (100) in accordance with MIL-R-47196.

B. Repair bracket subassembly (-50) as follows:

(1) Use an arbor press to remove two clinch nuts (55) from bracket (60). Discard two clinch
nuts (55).

(2) Use an arbor press to install two new clinch nuts (55) in bracket (60).

C. Repair bracket assembly (-65) as follows:

(1) Replace receptacle (75) as follows:

(a) Drill out two rivets (80) and remove receptacle (75) from bracket (90). Discard
receptacle (75).

(b) Position new receptacle (75) on bracket (90) and align holes.

(c) Install two new rivets (80) on bracket (90) in accordance with MIL-R-47196.

(2) Replace clinch nuts (85) as follows:

(a) Use an arbor press to remove two clinch nuts (85) from bracket (90). Discard two clinch
nuts (85).

(b) Use an arbor press to install two new clinch nuts (85) in bracket (90).

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PART NUMBER 60-1321

6. Repair of Battery Assembly.

NOTE: Refer to IPL Figure 1 for an illustration. Numbers in parentheses ( ) refer to item numbers
on the illustration.

A. Replace insulator (130) as follows:

(1) Use a soldering iron to disconnect two wires from insulator (130). Discard insulator (130).

(2) Use a soldering iron and electrical solder to solder two wires to insulator (130).

B. Replace electrical wiring as follows:

(1) Use a soldering iron to disconnect two wires from insulator (130) and two contacts on
housing (295). Discard wires.

(2) Slide a 1.5-inch (38 mm) piece of heat shrink tubing (M23053-5-104-0) over a 3-inch (76 mm)
piece of electrical wire (WI-348).

(3) Use a soldering iron and electrical solder to solder electrical wire prepared in step (2) to contact
on housing (295) and insulator (130).

(4) Use a heat gun to secure heat shrink tubing (M23053-5-104-0) in place.

(5) Use a soldering iron and electrical solder to solder a 7-inch (178 mm) piece of electrical wire
(WI-954) to contact on housing (295) and insulator (130).

7. Repair of Housing Subassembly.

NOTE: Refer to the IPL for illustrations. Numbers in parentheses ( ) refer to item numbers on the
illustration.

A. Replace resistor (R1) (5, IPL Figure 2) as follows:

(1) Use a sharp knife to remove heat shrink tubing from two terminals of resistor (R1) (5).

(2) Cut two electrical wires at base of resistor (R1) (5) terminals.

(3) Remove two stopnuts (15), screws (10) and resistor (R1) (5) from housing (160). Discard
resistor (R1) (5).

(4) Position new resistor (R1) (5) on housing (160) and secure with two screws (15) and
stopnuts (10).

(5) Slide two 0.5-inch (12,7 mm) pieces of heat shrink tubing (TU-285) over two electrical wires.

(6) Strip 0.25 inch (6,35 mm) of insulation from ends of two electrical wires leading to new
resistor (R1) (5).

(7) Use a soldering iron and electrical solder to connect two electrical wires to new
resistor (R1) (5).

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COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

(8) Slide heat shrink tubing (TU-285) over solder connections and use a heat gun to secure them
in place.

B. Repair connector (J1) (45) as follows:

(1) Remove four stopnuts (55), screws (50) and connector (J1) (45) from housing (160).

(2) Remove three seal plugs from connector (J1) (45). Discard seal plugs if damaged.

(3) Use an extraction/insertion tool to remove 12 contacts from connector (J1) (45). Discard
connector (J1) (45) if damaged.

(4) Cut 12 electrical wires at base of contacts. Discard contacts.

(5) Strip 0.25 inch (6,35 mm) of insulation from ends of 12 electrical wires leading to
connector (J1) (45).

(6) Use a crimping tool (M22520/1-01) to install 12 new contacts (M39029/31-241) on 12 electrical
wires.

(7) Use an extraction/insertion tool to install 12 new contacts (M39029/31-241) and electrical wires
in connector (J1) (45).

(8) Install three new seal plugs (MS27488-20) on connector (J1) (45).

(9) Position connector (J1) (45) on housing (160) and secure with four screws (50) and
stopnuts (55).

C. Replace ground terminal as follows:

(1) Remove stopnut (75), washer (80) and terminal from housing (160).

(2) Cut electrical wire at base of terminal. Discard terminal.

(3) Strip 0.25 inch (6,35 mm) of insulation from ends of electrical wire leading to terminal.

(4) Use a crimping tool (47386) to install new terminal (TE-089) on electrical wire.

(5) Position new terminal (TE-089) and electrical wire on housing (160) and secure with
washer (80) and stopnut (75).

D. Repair terminal assembly as follows:

(1) Remove two screws (90) and terminal assembly (-85) from housing (160).

(2) Remove stopnut (100) and pin (95) from bracket (135). Discard pin (95) if damaged.

(3) Cut two electrical wires at the base of terminals (105).

(4) Use a soldering iron to remove two terminals (105) from banana plugs (110). Discard
terminals (105) and banana plugs (110) if damaged.

(5) Drill out rivet (120) and remove insulator (115) from bracket (135). Discard insulator (115) if
damaged.

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COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

(6) Use an arbor press to press out two clinch nuts (130) from bracket (135). Discard clinch
nuts (130).

(7) Use an arbor press to install two clinch nuts (130) on bracket (135).

(8) Position new insulator (115) on bracket (135) and align holes.

(9) Install new rivet (120) in accordance with MIL-R-47196.

(10) Position new banana plug (110) and new terminal (105) on new insulator (115).

(11) Use a soldering iron and electrical solder to secure new terminal (105) and new banana
plug (110) to new insulator (115).

(12) Repeat steps (10) and (11) for remaining new banana plug (110) and new terminal (105).

(13) Strip 0.25 inch (6,35 mm) of insulation from ends of electrical wire leading to two new
terminals (105).

(14) Use a soldering iron and electrical solder to install two electrical wires on new terminals (105).

(15) Position new pin (95) on bracket (135) and secure with stopnut (100).

(16) Position terminal assembly (-85) on housing (160) and secure with two screws (90).

E. Repair printed circuit card assembly (20) as follows:

(1) Remove four stopnuts (30), spacers (35), screws (25), printed circuit card assembly (20) and
insulator (40) from housing (160).

(2) Replace terminal(s) (110, IPL Figure 3) as follows:

(a) Use a soldering iron to remove electrical wire from damaged terminal(s) (110).

(b) Use a soldering iron to remove terminal(s) (110) from printed wiring board (190). Discard
terminal(s) (110).

(c) Position new terminal(s) (110) on printed wiring board (190).

(d) Use a soldering iron and electrical solder to solder new terminal(s) (110) to printed wiring
board (190).

WARNING: CONFORMAL COATING IS FLAMMABLE AND TOXIC TO EYES, SKIN

AND RESPIRATORY TRACT. SKIN AND EYE PROTECTION
REQUIRED. AVOID REPEATED OR PROLONGED CONTACT. USE
ONLY IN WELL-VENTILATED AREAS. KEEP AWAY FROM OPEN
FLAMES OR OTHER SOURCES OF IGNITION.

(e) Apply conformal coating to repair areas. Allow to air dry for 4 hours.

(3) Replace rectifier (SCR1) (15) as follows:

(a) Use a soldering iron to disconnect rectifier (SCR1) (15).

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COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

(b) Remove rectifier (SCR1) (15) and mounting pad (20) from printed wiring board (190).
Discard rectifier (SCR1) (15).

(c) Position new rectifier (SCR1) (15) and mounting pad (20) on printed wiring board (190).

(d) Use a soldering iron and electrical solder to solder new rectifier (SCR1) (15) to printed
wiring board (190).

WARNING: CONFORMAL COATING IS FLAMMABLE AND TOXIC TO EYES, SKIN

AND RESPIRATORY TRACT. SKIN AND EYE PROTECTION
REQUIRED. AVOID REPEATED OR PROLONGED CONTACT. USE
ONLY IN WELL-VENTILATED AREAS. KEEP AWAY FROM OPEN
FLAMES OR OTHER SOURCES OF IGNITION.

(e) Apply conformal coating to repair areas. Allow to air dry for 4 hours.

(4) Replace transistors (Q1 and Q3) (145), (Q2) (60) and (Q4) (125) as follows:

(a) Use a soldering iron to disconnect transistor (Q1) (145) from printed wiring board (190).

(b) Remove transistor (Q1) (145) and mounting pad (150) from printed wiring board (190).
Discard transistor (Q1) (145).

(c) Position new transistor (Q1) (145) and mounting pad (150) on printed wiring board (190).

(d) Use a soldering iron and electrical solder to solder the leads of new transistor (Q1) (145)
to printed wiring board (190).

WARNING: CONFORMAL COATING IS FLAMMABLE AND TOXIC TO EYES, SKIN

AND RESPIRATORY TRACT. SKIN AND EYE PROTECTION
REQUIRED. AVOID REPEATED OR PROLONGED CONTACT. USE
ONLY IN WELL-VENTILATED AREAS. KEEP AWAY FROM OPEN
FLAMES OR OTHER SOURCES OF IGNITION.

(e) Apply conformal coating to repair areas. Allow to air dry for 4 hours.

(f) Repeat steps (a) through (e) for transistors (Q3) (145), (Q2) (60) and (Q4) (125) and
mounting pads (65), (150) and (130) as necessary.

(5) Replace terminal connected to transistor (Q5) (75) as follows:

(a) Remove self-locking nut (90), lockwasher (85) and terminal from transistor (Q5) (75).

(b) Cut electrical wire at the base of terminal. Discard terminal.

(c) Strip 0.25 inch (6,35 mm) of insulation from end of electrical wire.

(d) Use a crimping tool (47386) to install new terminal (TE-089) on electrical wire.

(e) Position new terminal (TE-089) on transistor (Q5) (75) and secure with lockwasher (85)
and self-locking nut (90).

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COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

(6) Replace transistor (Q5) (75) as follows:

(a) Use a soldering iron to unsolder transistor (Q5) (75) from printed wiring board (190).

(b) Remove two self-locking nuts (90), lockwashers (85), screws (80), terminal,
transistor (Q5) (75) and heat sink (100) from printed wiring board (190). Discard
transistor (Q5) (75).

(c) Position heat sink (100) and new transistor (Q5) (75) on printed wiring board (190) and
secure with two screws (80), terminal, two lockwashers (85) and self-locking nuts (90).

(d) Use a soldering iron and electrical solder to solder new transistor (Q5) (75) to printed
wiring board (190).

WARNING: CONFORMAL COATING IS FLAMMABLE AND TOXIC TO EYES, SKIN

AND RESPIRATORY TRACT. SKIN AND EYE PROTECTION
REQUIRED. AVOID REPEATED OR PROLONGED CONTACT. USE
ONLY IN WELL-VENTILATED AREAS. KEEP AWAY FROM OPEN
FLAMES OR OTHER SOURCES OF IGNITION.

(e) Apply conformal coating to repair areas. Allow to air dry for 4 hours.

(7) Replace capacitor (C3) (40) as follows:

(a) Use a soldering iron to remove capacitor (C3) (40) from printed wiring board (190).
Discard capacitor (C3) (40).

WARNING: ADHESIVE IS HIGHLY FLAMMABLE. AVOID INHALATION OF VAPORS

AND CONTACT WITH SKIN. OBSERVE FIRE PRECAUTIONS.

(b) Apply adhesive (AD-040) to mating surfaces of new capacitor (C3) (40) and printed wiring
board (190).

(c) Install new capacitor (C3) (40) on printed wiring board (190). Use a clean cloth to remove
excess adhesive. Allow to air dry for 4 hours.

(d) Use a soldering iron and electrical solder to solder capacitor (C3) (40) to printed wiring
board (190).

WARNING: CONFORMAL COATING IS FLAMMABLE AND TOXIC TO EYES, SKIN

AND RESPIRATORY TRACT. SKIN AND EYE PROTECTION
REQUIRED. AVOID REPEATED OR PROLONGED CONTACT. USE
ONLY IN WELL-VENTILATED AREAS. KEEP AWAY FROM OPEN
FLAMES OR OTHER SOURCES OF IGNITION.

(e) Apply conformal coating to repair areas. Allow to air dry for 4 hours.

(8) Replace resistors (R8) (55) and (R13) (140) as follows:

(a) Use a soldering iron to remove resistors (R8) (55) and (R13) (140) from printed wiring
board (190). Discard resistors (R8) (55) and (R13) (140).

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

(b) Mount new resistors (R8) (55) and (R13) (140) 0.020 to 0.065 inch (0,51 to 1,65 mm) from
surface of printed wiring board (190).

(c) Use a soldering iron and electrical solder to solder new resistors (R8) (55) and (R13) (140)
to printed wiring board (190).

WARNING: CONFORMAL COATING IS FLAMMABLE AND TOXIC TO EYES, SKIN

AND RESPIRATORY TRACT. SKIN AND EYE PROTECTION
REQUIRED. AVOID REPEATED OR PROLONGED CONTACT. USE
ONLY IN WELL-VENTILATED AREAS. KEEP AWAY FROM OPEN
FLAMES OR OTHER SOURCES OF IGNITION.

(d) Apply conformal coating to repair areas. Allow to air dry for 4 hours.

(9) Replace electrical wire as follows:

(a) Remove self-locking nut (90), lockwasher (85) and terminal with wire from
transistor (Q5) (75).

(b) Use a soldering iron to remove electrical wire from printed wiring board (190). Discard
electrical wire.

(c) Strip 0.25 inch (6,35 mm) of insulation from ends of a 2.125-inch (53,98 mm) piece of
electrical wire (WI-502).

(d) Use a crimping tool (47386) to install new terminal (TE-089) on one end of electrical wire
(WI-502).

(e) Position new terminal (TE-089) and electrical wire (WI-502) on transistor (Q5) (75) and
secure with lockwasher (85) and self-locking nut (90).

(f) Use a soldering iron and electrical solder to solder other end of electrical wire (WI-502) to
printed wiring board (190).

WARNING: CONFORMAL COATING IS FLAMMABLE AND TOXIC TO EYES, SKIN

AND RESPIRATORY TRACT. SKIN AND EYE PROTECTION
REQUIRED. AVOID REPEATED OR PROLONGED CONTACT. USE
ONLY IN WELL-VENTILATED AREAS. KEEP AWAY FROM OPEN
FLAMES OR OTHER SOURCES OF IGNITION.

(g) Apply conformal coating to repair areas. Allow to air dry for 4 hours.

(10) Replace bus wire as follows:

(a) Use a soldering iron to remove bus wire and tubing from component side of printed wiring
board (190). Discard bus wire and tubing.

(b) Place a 0.313-inch (7,95 mm) piece of tubing (TU-170) over a 1-inch (25 mm) piece of bus
wire (WI-646).

(c) Use a soldering iron and electrical solder to solder bus wire to component side of printed
wiring board (190).

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

(d) Use a soldering iron to remove bus wire and tubing from solder side of printed wiring
board (190). Discard bus wire and tubing.

(e) Place a 1.25-inch (31,8 mm) piece of tubing (TU-170) over a 1.75-inch (44,5 mm) piece of
bus wire (WI-646).

(f) Use a soldering iron and electrical solder to solder bus wire to solder side of printed wiring
board (190).

WARNING: CONFORMAL COATING IS FLAMMABLE AND TOXIC TO EYES, SKIN

AND RESPIRATORY TRACT. SKIN AND EYE PROTECTION
REQUIRED. AVOID REPEATED OR PROLONGED CONTACT. USE
ONLY IN WELL-VENTILATED AREAS. KEEP AWAY FROM OPEN
FLAMES OR OTHER SOURCES OF IGNITION.

(g) Apply conformal coating to repair areas. Allow to air dry for 4 hours.

(11) Position circuit card assembly (20, IPL Figure 2) and insulator (40) in housing (160) and secure
with four screws (25), spacers (35) and stopnuts (30).

F. Repair circuit card assembly (140) as follows:

(1) Remove four stopnuts (150), spacers (155), screws (145) and circuit card assembly (140) from
housing (160).

(2) Replace capacitors (C6) (5, IPL Figure 4) and (C7) (50) as follows:

(a) Use a soldering iron to remove capacitors (C6) (5) and (C7) (50) from printed wiring board
(55). Discard capacitors (C6) (5) and (C7) (50).

WARNING: PRIMER AND ADHESIVE IS HIGHLY FLAMMABLE. AVOID INHALATION

OF VAPORS AND CONTACT WITH SKIN. OBSERVE FIRE
PRECAUTIONS.

(b) Apply primer (AD-059) and adhesive (AD-053) to mating surfaces of new
capacitors (C6) (5) and (C7) (50) and printed wiring board (55).

(c) Position capacitors new (C6) (5) and (C7) (50) on printed wiring board (55).

(d) Use a soldering iron and electrical solder to solder new capacitors (C6) (5) and (C7) (50)
to printed wiring board (55). Use a clean cloth to remove excess primer and adhesive.
Allow to air dry for 4 hours.

WARNING: CONFORMAL COATING IS FLAMMABLE AND TOXIC TO EYES, SKIN

AND RESPIRATORY TRACT. SKIN AND EYE PROTECTION
REQUIRED. AVOID REPEATED OR PROLONGED CONTACT. USE
ONLY IN WELL-VENTILATED AREAS. KEEP AWAY FROM OPEN
FLAMES OR OTHER SOURCES OF IGNITION.

(e) Apply conformal coating to repair areas. Allow to air dry for 4 hours.

(3) Replace transistors (Q6) (15) and (Q7) (10) as follows:

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

(a) Use a soldering iron to disconnect transistors (Q6) (15) and (Q7) (10) from printed wiring
board (55).

(b) Remove transistors (Q6) (15) and (Q7) (10) and two mounting pads (20) from printed
wiring board (55). Discard transistors (Q6) (15) and (Q7) (10).

(c) Position new transistors (Q6) (15) and (Q7) (10) and two mounting pads (20) on printed
wiring board (55).

(d) Use a soldering iron and electrical solder to solder leads of new transistors (Q6) (15)
and (Q7) (10) to printed wiring board (55).

WARNING: CONFORMAL COATING IS FLAMMABLE AND TOXIC TO EYES, SKIN

AND RESPIRATORY TRACT. SKIN AND EYE PROTECTION
REQUIRED. AVOID REPEATED OR PROLONGED CONTACT. USE
ONLY IN WELL-VENTILATED AREAS. KEEP AWAY FROM OPEN
FLAMES OR OTHER SOURCES OF IGNITION.

(e) Apply conformal coating to repair areas. Allow to air dry for 4 hours.

(4) Position circuit card assembly (140, IPL Figure 2) and four spacers (155) in housing (160) and
secure with four screws (145) and stopnuts (150).

G. Replace electrical wiring as follows:

NOTE: Tag electrical wires before disconnecting for ease of assembly.

(1) Remove stopnut (75), washer (80) and terminal from housing (160).

(2) Use a sharp knife to remove heat shrink tubing from two terminals of resistor (R1) (5).

(3) Use a soldering iron to remove damaged electrical wire(s) from resistor (R1) (5).

(4) Use a sharp knife to remove heat shrink tubing from two wires leading from resistor (R1) (5).

(5) Remove four stopnuts (55), screws (50) and connector (J1) (45) from housing (160).

(6) Use an extraction/insertion tool to remove damaged wire(s) and contact(s) from
connector (J1) (45).

(7) Use a soldering iron to remove damaged electrical wire(s) from circuit card assembly (20).

(8) Use a soldering iron to remove damaged electrical wire(s) from circuit card assembly (140).

(9) Remove self-locking nut (90, IPL Figure 3), lockwasher (85) and terminal and electrical wire
from printed circuit card assembly (20, IPL Figure 2).

(10) Remove two screws (90) and terminal assembly (-85) from housing (160).

(11) Use a soldering iron to remove damaged electrical wires from terminal(s) (105).

(12) Remove damaged electrical wires as needed.

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

(13) Position new electrical wires as needed. Refer to Figure 604 and Table 1 for wiring diagrams.
Refer to Table 603 and Table 604 for wire lists for the power supply.

(14) Strip 0.25 inch (6,35 mm) from ends of new electrical wires.

(15) Use a soldering iron and electrical solder to solder new electrical wire(s) to terminal(s) (105,
IPL Figure 2).

(16) Position terminal assembly (-85) and secure with two screws (90).

(17) Use a crimping tool (47386) to install new terminal (TE-089) on new electrical wire.

(18) Position new terminal (TE-089) on printed circuit card assembly (20) and secure with
lockwasher (85, IPL Figure 3) and self-locking nut (90).

(19) Use a soldering iron and electrical solder to solder new electrical wire(s) to printed circuit card
assembly (20, IPL Figure 2).

(20) Use a soldering iron and electrical solder to solder new electrical wire(s) to circuit card
assembly (140).

WARNING: CONFORMAL COATING IS FLAMMABLE AND TOXIC TO EYES, SKIN AND

RESPIRATORY TRACT. SKIN AND EYE PROTECTION REQUIRED. AVOID
REPEATED OR PROLONGED CONTACT. USE ONLY IN WELL-
VENTILATED AREAS. KEEP AWAY FROM OPEN FLAMES OR OTHER
SOURCES OF IGNITION.

(21) Apply conformal coating to repair areas. Allow to air dry for 4 hours.

(22) Use a crimping tool (M22520/1-01) to install new contact(s) (M39029/31-241) on new electrical
wire(s) leading to connector (J1) (45).

(23) Use an extraction/insertion tool to install contact(s) (M39029/31-241) in connector (J1) (45).

(24) Position connector (J1) (45) in housing (160) and secure with four screws (50) and
stopnuts (55).

(25) Slide a 1.0-inch (25,4 mm) piece of heat shrink tubing (TU-285) over two new electrical wires
leading to resistor (R1) (5).

(26) Slide two 0.5-inch (12,7 mm) pieces of heat shrink tubing (TU-285) over two new electrical
wires leading to resistor (R1) (5).

(27) Use a soldering iron and electrical solder to solder two electrical wires to resistor (R1) (5).

(28) Slide two 0.5-inch (12,7 mm) pieces of heat shrink tubing (TU-285) over solder connections
and use a heat gun to secure in place.

(29) Slide 1.0-inch (25,4 mm) piece of heat shrink tubing (TU-285) into place and use a heat gun to
secure.

(30) Use a crimping tool (47386) to install new terminal (TE-089) on new electrical wire.

(31) Position new terminal (TE-089) on housing (160) and secure with washer (80) and stopnut (75).

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

Power Supply P/Ns 60-1321-1 and -5 Wiring Diagram

Figure 604

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

Table 603. Power Supply P/Ns 60-1321-1 and -5 Wire List

WIRE DESCRIPTION LENGTH FROM TO

NO.
1 Yellow (22AWG) 3.5 inches (89 mm) Point 16 Connector (J1), Pin 1
2 Yellow (22AWG) 3.5 inches (89 mm) Point 5 Connector (J1), Pin 2
3 Yellow (22AWG) 3.5 inches (89 mm) Point 2 Connector (J1), Pin 3
4 Yellow (22AWG) 7.5 inches (191 mm) Point 15 Connector (J1), Pin 4
5 Black (22AWG) 5 inches (127 mm) Point 4 Connector (J1), Pin 5
6 Yellow (22AWG) 6.5 inches (165 mm) Point 8 Connector (J1), Pin 6
7 Black (22AWG) 11 inches (279 mm) Point 4 Point 12
8 Yellow (22AWG) 6.5 inches (165 mm) Point 9 Connector (J1), Pin 8
9 Brown (22AWG) 4.0 inches (102 mm) Point 7 Point 6
10 Yellow (22AWG) 7.5 inches (191 mm) Point 10 Connector (J1), Pin 10
11 Brown (22AWG) 9 inches (229 mm) Point 14 Point 13
12 Yellow (22AWG) 7.5 inches (191 mm) Point 11 Connector (J1), Pin 12
13 Black (22AWG) 4.0 inches (102 mm) Point 11 Point 12
14 Brown (22AWG) 4.0 inches (102 mm) Point 1 Point 3

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

Power Supply P/N 60-1321-7 Wiring Diagram

Figure 605

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

Table 604. Power Supply P/N 60-1321-7 Wire List

WIRE DESCRIPTION LENGTH FROM TO

NO.
1 Yellow (22AWG) 7 inches (178 mm) CCA (140), Point 4 Connector (J1), Pin 2
2 Yellow (22AWG) 3.5 inches (89 mm) CCA (20), Point 2 Connector (J1), Pin 3
3 Yellow (22AWG) 7.5 inches (191 mm) CCA (20), Point 15 Connector (J1), Pin 4
4 Black (22AWG) 3 inches (76 mm) CCA (20), Point 4 Connector (J1), Pin 5
5 Yellow (22AWG) 6.5 inches (165 mm) CCA (20), Point 8 Connector (J1), Pin 6
6 Yellow (22AWG) 6.5 inches (165 mm) CCA (20), Point 9 Connector (J1), Pin 8
7 Yellow (22AWG) 7 inches (178 mm) CCA (140), Point 1 Connector (J1), Pin 9
8 Yellow (22AWG) 7.5 inches (191 mm) CCA (20), Point 10 Connector (J1), Pin 10
9 Yellow (22AWG) 7.5 inches (191 mm) CCA (20), Point 11 Connector (J1), Pin 12
10 Black (22AWG) 8.5 inches (216 mm) CCA (20), Point 4 Point 12
11 Brown (22AWG) 3 inches (76 mm) Point 7 CCA (20), Point 6
12 Black (22AWG) 4.0 inches (102 mm) Point 17 Point 12
13 Brown (22AWG) 5 inches (127 mm) Point 1 CCA (20), Point 3
14 Brown (22AWG) 9 inches (229 mm) CCA (20), Point 14 Point 13
15 Orange (22AWG) 1.5 inches (38 mm) CCA (20), Point 14 CCA (140), Point 2
16 Green (22AWG) 6 inches (152 mm) CCA (20), Point 5 CCA (140), Point 3
17 Violet (22AWG) 5 inches (127 mm) CCA (20), Point 18 CCA (140), Point 5
18 Gray (22AWG) 5.5 inches (140 mm) CCA (20), Point 19 CCA (140), Point 6

8. Replacement of Identification Plates or Identification Labels.

NOTE: Grimes Aerospace Company does not authorize replacement of the identification plate
(10, IPL Figure 1) or identification label (310). For further information, contact a Grimes
Aerospace representative at the following address:

Grimes Aerospace Co.

550 State Route 55
Urbana, OH 43078-1059
Telephone: (937) 484-2000
FAX: (937) 484-2101
SITA: DAYFLCR

A. If illegible, remove and replace instruction plate (5) or instruction label (305) on cover subassembly
(-15).

B. If illegible, remove and replace static caution label (315) on housing assembly (300).

C. If illegible, remove and replace MOD labels (320) on outside and inside of housing assembly (300).

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

9. Postrepair Procedures.

A. Clean parts. Refer to CLEANING, section 401, for details.

B. Wrap parts in a clean cloth to avoid contamination until ready for assembly.

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COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

ASSEMBLY (INCLUDING STORAGE)

1. General Information.

A. The following paragraphs provide information for assembly (including storage) of the power supply.

B. Examine the parts for damage. Refer to CHECK, section 501, for details.

C. Repair the parts before assembly. Refer to REPAIR, section 601, for details.

D. Refer to Table 701 for a list of materials needed for assembly (including storage). Equivalent
substitutes are acceptable.

Table 701. Materials List

NOMENCLATURE SPECIFICATION MANUFACTURER

Adhesive (AD-053*) 738 Dow Corning Corp.
Midland, MI (V71984)
Adhesive (AD-300*) 84 Loctite Corp.
Rocky Hill, CT (V05972)
Cleaning Cloth A-A-59323 Commercially Available
Cushion and Dunnage PPP-C-1752, Unicellular, Commercially Available
Polyethylene Foam
Desiccant MIL-D-3464 Commercially Available
Masking Tape 0.75-Inch Wide Commercially Available
Plastic Bag None Commercially Available
Wrapping Material MIL-B-121, Grade A Commercially Available
Unit Container PPP-B-636, Type CF or SF, Commercially Available
Class Weather Resistant
*Grimes reference only.

2. Assembly of Cover Assembly.

NOTE: Refer to IPL Figure 1 for an illustration. Numbers in parentheses ( ) refer to item numbers on
the illustration.

A. Position bracket assembly (-65) on cover plate (110) and secure with two screws (70).

B. Position two bracket subassemblies (-50) on cover plate (110) and secure with four screws (35).

C. Position two receptacles (40) on bracket subassemblies (-50) and secure with locknut (45).

D. Position four studs (20) on cover plate (110) and secure with washers (25).

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

3. Assembly of Battery Assembly.

NOTE: Refer to IPL Figure 1 for an illustration. Numbers in parentheses ( ) refer to item numbers on
the illustration.

A. Place two cushioning pads (190) on battery subassembly (BT1) (275).

WARNING: ADHESIVE IS HIGHLY FLAMMABLE. AVOID INHALATION OF VAPORS AND

CONTACT WITH SKIN. OBSERVE FIRE PRECAUTIONS.

B. Place a bead of adhesive (AD-053) on housing (185) where battery subassembly (BT1) (275) will be
positioned.

C. Position battery subassembly (BT1) (275) on housing (185). Use a clean cloth to remove excess
adhesive. Allow to air dry for 4 hours.

WARNING: ADHESIVE IS HIGHLY FLAMMABLE. AVOID INHALATION OF VAPORS AND

CONTACT WITH SKIN. OBSERVE FIRE PRECAUTIONS.

D. Position housing (295) on housing (185). Apply adhesive (AD-300) to threads of six screws (175)
and secure housing (295) to housing (185). Use a clean cloth to remove excess adhesive. Allow to
air dry for 4 hours.

E. Position insulator (130) on support (165) and secure with screw (135), washer (140) and
stopnut (145).

F. Position two studs (160) and stud (155) on support (165) and secure with three washers (150).

G. Position support (165) on battery assembly (-115A) and secure with four screws (125).

4. Assembly of Power Supply.

NOTE: Refer to IPL Figure 1 for an illustration. Numbers in parentheses ( ) refer to item numbers on
the illustration.

A. Position cover subassembly (-15) on battery assembly (-115A) and secure by tightening studs (155)
and (160).

B. Position battery assembly (-115A) and cover subassembly (-15) on housing assembly (300) and
secure by tightening four studs (20).

C. Test power supply. Refer to TESTING AND FAULT ISOLATION, section 101, for details.

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

5. Storage.

NOTE: Refer to IPL Figure 1 for an illustration. Numbers in parentheses ( ) refer to item numbers
on the illustration.

A. General conditions for battery storage.

(1) Subjection to extreme variations in temperature during storage or shipment will cause some
loss of charge due to “self-discharge” characteristics of nickel-cadmium cells.

(2) Storage temperatures should not go below -40 °F (-40 °C) or more than 165 °F (74 °C) to
prevent damage to cell structures. At storage temperatures above 100 °F (37.78 °C), self-
discharge will increase considerably compared to self-discharge at 68 °F (20 °C). Cold storage
at 32 °F (0 °C) offers definite improvement of charge retention and is recommended when
practical.

(3) Self-discharge of cells may be minimized by storage at 32 °F (0 °C) with a loss of

approximately 10% of available capacity after 50 days storage. Storage at 68 °F (20 °C) will
produce a 50% loss in available power after a storage period of 50 days. Fully charged battery
assemblies stored at 32 °F (0 °C) for up to 50 days may normally be placed in service without
further charging. Fully charged battery assemblies stored at no more than 68 °F (20 °C) for up
to 7 days may normally be placed in service without further charging.

B. Storage for line maintenance.

(1) Power supplies or battery assemblies in a fully charged state may be stored under the following
controlled conditions and placed into immediate service without additional charging:

(a) Storage at 68 °F (20 °C) for a period of 7 days or less.

(b) Storage at 32 °F (0 °C) for a period of 50 days or less.

(c) Trickle-charge storage for up to six months.

C. Storage for other than line maintenance.

(1) Battery assemblies may be stored in the power supply or removed from the power supply.

(2) Battery assemblies may be stored at -4 °F (-20 °C) to 122 °F (50 °C) for an indefinite storage
period.

D. Charging of battery assembly (BT1) (275) after storage.

(1) Power supply and battery assembly (BT1) (275) removed from storage should be inspected for
visible damage. Battery terminals and contacts should be cleaned prior to charging. A white
deposit present on battery terminals and/or contacts is not abnormal and may be removed with
a clean cloth dampened with warm water.

(2) Apply a constant DC current of 265 mA to battery assembly (BT1) (275) for 16 to 20 hours.

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COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

(3) At completion of the charging operation, and with the power supply still on charge, battery
assembly (BT1) (275) shall measure a minimum of 8.4 Vdc. If less than 8.4 Vdc is measured,
continue the charging operation for an additional 4 hours.

(4) If the battery assembly (BT1) (275) still does not measure a minimum of 8.4 Vdc, replace
battery assembly (BT1) (275).

E. Trickle-charge storage.

(1) Fully charged battery assembly (BT1) (275) may be stored under trickle-charge condition for up
to six months and be placed into immediate service without additional charging.

(2) Storage temperature must not exceed 100 °F (38 °C).

(3) A battery assembly (BT1) (275) stored under trickle-charge condition in excess of six months
should not be immediately placed in service. Instead, battery assembly (BT1) (275) should be
removed and discharged under a 2-amp load down to 0.9 Vdc per cell and then charged for 24
hours.

NOTE: Battery cells should be individually loaded and measured to detect shorted or
reverse-charged cells.

(4) To trickle-charge battery assembly (BT1) (275), apply a constant current of 100 mA dc.

F. Pack the power supply as follows:

(1) Wipe the power supply with a clean cloth to remove dirt, dust and foreign material.

(2) Preserve the power supply in accordance with MIL-P-116, Method 1-A-8.

(3) Wrap the power supply in wrapping material and place in plastic bag.

(4) Place cushion and dunnage material, desiccant and the power supply in unit container, then
seal with masking tape.

(5) Mark outside of unit container in accordance with MIL-STD-129. Also include overhaul date and
location.

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

SPECIAL TOOLS, FIXTURES AND EQUIPMENT

1. General Information.

A. The following paragraphs provide information for special tools, fixtures and equipment used for
overhaul of the power supply.

B. Refer to Table 901 for a list of this equipment. These items may be purchased from Grimes
Aerospace Company, the original manufacturer or, in some cases, locally manufactured. Refer to
the referenced figure for details. Equivalent substitutes are acceptable.

Table 901. Special Tools, Fixtures and Equipment List

NOMENCLATURE PART/MODEL USED FOR FIGURE

NUMBER NUMBER
Arbor Press Drake Model 3A Repair NA
MSC Industrial
Supply Co.
Jonestown, PA (V08NV1)
Crimping Tool M22520/1-01 Repair NA
Crimping Tool 47386 Repair NA
Amp, Inc.
Middletown, PA (V00779)
Digital Multimeter Model 87 Testing and NA
(DMM) (0 to 200 V, Fluke Corp. Fault Isolation
0 to 2000 mA, Everett, WA (V89536)
Accuracy ±1%)
(Qty. 2)
Extraction/Insertion Tool TH554 FT8 Electrical Contact NA
Daniels Mfg. Corp. Replacement
Orlando, FL (V11851)
Heat Gun Commercially Available Heat Shrink Tubing NA
Soldering Iron Commercially Available Repair NA
Tester 71572 Testing and 901
Grimes Aerospace Co. Fault Isolation
Urbana, OH (V72914)
Tester 63845 Testing and 902
Grimes Aerospace Co. Fault Isolation
Urbana, OH (V72914)
Variable Regulated Commercially Available Testing and NA
Power Supply Fault Isolation
(0-45 Vdc, 6-amp min)
Variable Regulated Commercially Available Testing and NA
Power Supply Fault Isolation of P/N
(0-120 Vac, 400 Hz) 60-1321-7 only

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

Tester Schematic, P/N 71572

Figure 901

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

Tester Schematic, P/N 63845

Figure 902

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Oct 1/05
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

ILLUSTRATED PARTS LIST

1. General Information.

A. The Illustrated Parts List (IPL) provides a breakdown of assemblies, subassemblies and detail parts
of the power supply. All parts are listed, except for parts which lose their identities by being
permanently fastened to other parts or are part of an assembly not subject to disassembly.

B. Bulk materials such as backshells, contacts, ring terminals, safety or electrical wires, strain reliefs,
tape and Ty-Raps and consumable materials such as adhesives, sealants, lubricants, solder, paints
and primers are not included in the detailed parts lists. These materials are identified in the
materials list at the beginning of each section.

C. To find a part number when the part number is unknown, locate the part on the illustration and note
the item number. Locate the item number on the detailed parts list. The part number will be shown
on the same line. In some instances there are gaps in item number sequence and the item numbers
are not continuously sequential.

2. Explanation of Columns, Terms and Symbols in the Illustrated Parts List (IPL).

A. FIG. & ITEM NO. column: The figure and item numbers key the detailed parts list to the applicable
illustration. The first number represents the figure number of the illustration. The item number
corresponds to an item number on the illustration.

(1) An item number not on the illustration is identified by a dash (-) preceding the item number.
This can indicate the following:

(a) When two or more visually alike parts are listed in sequence, only the first part is
illustrated. The illustration, however, is applicable to both parts.

(b) When detail parts of an assembly or installation are separately illustrated, the resulting
assembly may be illustrated as an assembly by bracketing the detail parts and identifying
the bracket as the assembly. If brackets are not used, the detail parts are illustrated, but
the assembly is not.

(2) An item number followed by an alphabetical character such as A, B, C, etc., indicates the part
listed is similar to the same item number without the alphabetical character. The difference
could be each part is used for a different next higher assembly (NHA) or is an equivalent part.
This will be noted in the NOMENCLATURE or EFF CODE columns.

B. PART NUMBER column: This column contains the original manufacturer’s part number of the
assembly, subassembly or detail part listed. Part numbers in this IPL are those of Grimes
Aerospace Company, Urbana, Ohio (V72914) or are standard parts unless a Commercial and
Government Entity (CAGE) code appears in the NOMENCLATURE column. Refer to paragraph 4
for details. The following phrases may be used in this column:

„ “ORDER NHA” is used when no part number exists for the part listed or when it is preferable to
order an assembly rather than detail parts. ORDER NHA items which have no part numbers
are not procurable and should not be ordered. The next higher assembly, however, is
procurable and may be ordered.

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COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

„ “NONPROC” followed by an assigned number (for example NONPROC123) is used when no

part number exists for the assembly. NONPROC assemblies are not procurable and may not
be ordered. However, the detail parts of the assembly are procurable and may be ordered,
unless otherwise specified.

„ “REF” followed by an assigned number (for example REF001) is used when the part number is
more than fifteen digits. The original part number with more than fifteen digits is listed in the
NOMENCLATURE column and is the part number to be used when ordering the part.

C. AIRLINE STOCK NO. column: This column is reserved for airline part numbers and accommodates
eleven numbers.

D. NOMENCLATURE column: This column identifies the parts being listed by noun name followed by
modifiers when applicable. This includes assemblies which are not broken down within the IPL.
Assemblies which are broken down within the IPL will be listed in plain English. This column also
provides the following information:

(1) The relationship of each listed item to its next higher assembly (NHA) is shown by an indenture
code. Each listed item is placed in the NOMENCLATURE column one indenture (one dot) to
the right of the assembly to which it belongs. Items at equal indentures are all components of a
single assembly or subassembly. An example of the indenture code system is shown below:

1 2 3 4 5 6 7

Assembly or Installation Descriptive Title

. Assembly
. Attaching Parts for Assembly
. . Detail Parts for Assembly
. . . Subassembly
. . . Attaching Parts for Subassembly
. . . . Detail Parts for Subassembly
. . . . . Sub-Subassembly
. . . . . Attaching Parts for Sub-Subassembly
. . . . . . Detail Parts for Sub-Subassembly

(2) Symbols used, with the exception of effectivity and CAGE codes, are as follows:

(ATTACHING PARTS) Designates start of each group of attaching parts.

-------*------- Designates end of each group of attaching parts.

(3) The following phrases may be used in this column:

„ “DELETED” identifies a part no longer used.

„ “SUPSD” identifies a part no longer authorized for use; quantities will be listed as “NP.”
Example: (SUPSD BY ITEM XXX).

„ “SUPSDS” identifies the newer part to be used. Example: (SUPSDS ITEM XXX).

„ “REPLACES” or “REPLACES ITEM XXX” identifies this part is newer and therefore more
desirable than the “REPLACED” part. However, either may be used.

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

„ “REPLACED” or “REPL BY ITEM XXX” identifies this part is older and therefore less
desirable than the “REPLACES” part. However, either may be used.

„ “ALTN PART FOR ITEM XXX” identifies this part as an alternative. However, either part
may be used and neither is more desirable than the other.

„ “TPN” precedes a True Part Number with all dashes, slashes, spaces and/or symbols
assigned by the original manufacturer of the part. This is the part number to be used
when ordering the part.

E. EFF CODE column: This column establishes part relationship with assemblies, which are essentially
the same, but have minor variations. These assemblies are the end items on the detailed parts list
and are assigned reference letters such as A, B, C, D, etc. Subassemblies or detail parts, which are
not common to all configurations, but are associated with one or more of the coded end items, carry
the letter or letters assigned to the end item(s) with which they are associated. If a part is common
to all end items, the EFF CODE column is blank.

F. UNITS PER ASSY column: This column shows the quantity of each item required for the next higher
subassembly, assembly or installation outline. The quantity shown for attaching parts is the total
number required for the related part, subassembly or assembly and, therefore, may not be the total
quantity used for the end item of the detailed parts list. The following letters may be used in this
column:

„ “AR” indicates “as required” and refers to variable quantity items such as shims, spacers or
similar items.

„ “RF” indicates "reference" and refers to items and their quantities which are listed elsewhere
and are provided here as a reference only.

„ "NP" indicates "nonprocurable" and refers to items which are not procurable and may not be
ordered.

3. Abbreviations. Standard abbreviations used in the IPL agree with MIL-STD-12, except as noted below:

Abbreviation Definition

None

4. Commercial and Government Entity (CAGE) Codes.

A. CAGE codes, preceded by the capital letter "V" (V12345), are used to identify the original
manufacturer of non-Grimes Aerospace Company (V72914) components. CAGE codes are listed in
the NOMENCLATURE column, except for the Government codes below, which are not listed:

V96906 Military Standard (prefix MS)

V88044 Army/Navy Standard (prefix AN)
V80205 National Aircraft Standard (prefix NAS)

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

B. The following CAGE codes are listed in this IPL:

V01295 Texas Instruments, Inc. V56289 Sprague Electric Co.

Semiconductor Group World Hqs.
MS 8670 678 Main St.
8505 Forest Ln. Sanford, ME 04073
P.O. Box 660199
V71286 Fairchild Fasteners Camloc Products
Dallas, TX 75243
South Bay Opns.
V04713 Motorola, Inc. 3014 W. Lomita Blvd.
Semiconductor Products Sector Torrance, CA 90505-5103
MD 56126
V80539 SPS Technologies, Inc.
3102 N. 56th St.
Aerospace and Industrial Products
Phoenix, AZ 85018-6606
2701 S. Harbor Blvd.
V11815 Textron, Inc. Santa Ana, CA 92704-5803
Textron Aerospace Fasteners Div.
V83330 Dialight Corp.
1224 E. Warner Ave.
Manasquan Div.
Santa Ana, CA 92707-0157
1913 Atlantic Ave.
V13103 Thermalloy Co., Inc. Manasquan, NJ 08736-1005
2021 W. Valley View Ln.
V86577 Precision Metal Products Co.
P.O. Box 810839
Peabody, MA 01960
Dallas, TX 75381
V93790 Cornell-Dubilier Electronics
V14433 ITT Semiconductors Div.
1605 E. Rodney French Blvd.
West Palm Beach, FL 33401
New Bedford, MA 02741-9990
V15653 Kaynar Technologies, Inc.
V96791 Bunker Ramo Corp.
Kaynar Div.
Amphenol Controls Div.
800 S. State College Blvd.
Janesville, WI 53545
Fullerton, CA 92831-3001
V18310 Concord Electronics Corp.
30 Great Jones St.
New York, NY 10012

5. Overhaul. The power supply may be returned to Grimes Aerospace (V72914) for overhaul. For further
information, contact a Grimes Aerospace representative at the following address:

Grimes Aerospace Co.

550 State Route 55
Urbana, OH 43078-1059
Telephone: (937) 484-2000
FAX: (937) 484-2101
SITA: DAYFLCR

6. Numeric Index (NI). Refer to Table 1001.

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

Table 1001. Numeric Index (Sheet 1 of 7)

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NO. NUMBER NO. REQUIRED
AN960C4 1 140 1
A2578 1 105 NP
A2578-3 1 -105 2
A3905 2 35 4
A3905 2 155 4
K7000-04-9 2 130 2
MS20426A3-5 1 80 2
MS20426A3-6 2 120 1
MS20426A4-5 1 100 4
MS210404 2 150 NP
MS21042-04 1 145 1
MS21042-04 2 30 NP
MS21042-04 2 55 NP
MS21042-06 2 75 1
MS21042-06 2 100 NP
MS21042-06 3 90 2
MS21042L04 2 -30A 4
MS21042L04 2 -55A 4
MS21042L04 2 -150A 4
MS21042L06 2 -100A 1
MS24264R12B12PN 2 -45A 1
MS24264R12B12PX 2 45 NP
MS24693C2 2 -90A 2
MS24693C4 1 -35B 2
MS24693C4 1 -70B 2
MS24693S2 2 90 NP
MS24693S3 1 35 NP
MS24693S3 1 70 NP
MS24693S4 1 -35A NP
MS24693S4 1 -70A NP

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

Table 1001. Numeric Index (Sheet 2 of 7)

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NO. NUMBER NO. REQUIRED
MS27183-2 1 -215
MS27183-2 1 -240
MS27183-2 1 -265
MS27488-20 2 -65
MS35190-212 1 -200
MS35190-212 1 -225
MS35190-212 1 -250
MS35190-226 1 175 6
MS35206-203 2 10 NP
MS35206-213 1 125 4
MS35206-213 2 50 NP
MS35206-214 2 -50A NP
MS35206-216 2 25 NP
MS35206-217 2 -25A NP
MS35206-217 2 145 NP
MS35206-219 1 135 1
MS35206-229 3 80 2
MS35206-230 3 -80A
MS35338-39 1 -210
MS35338-39 1 -235
MS35338-39 1 -260
MS35338-41 3 85 2
MS35649-222 1 -205
MS35649-222 1 -230
MS35649-222 1 -255
MS51957-14 2 -50B 4
MS51957-17 2 -25B 4
MS51957-17 2 -145A 4
MS51957-3 2 -10A 2

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

Table 1001. Numeric Index (Sheet 3 of 7)

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NO. NUMBER NO. REQUIRED
M38527-004N 4 20 NP
M38527-02-004N 4 -20A 2
M38527-08-041P 3 -20A 1
M38527-08-041P 3 -65A 1
M38527-08-041P 3 -130A 1
M38527-08-041P 3 -150A 2
M39029-31-241 2 -60
M45938-6-4 1 55 2
M45938-6-4 1 85 2
NAS620-6L 2 80 1
N41D188-440 1 180 3
N41D188-440 1 290 7
ORDER NHA 1 60 NP
ORDER NHA 1 90 NP
ORDER NHA 1 185 NP
ORDER NHA 1 295 NP
ORDER NHA 2 135 NP
S106 1 -270
WMF1S47K 3 35 1
1N4385 3 175 1
1N4385 3 180 1
1N4385 4 45 2
1N5231B 3 120 1
10-401-2-01 3 -110A 11
10-401-2-01 3 -110B 12
10-401-2-01 3 -110C 13
121 2 110 2
150D476X9035S2 3 40 1
150D476X9035S2 4 50 NP

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

Table 1001. Numeric Index (Sheet 4 of 7)

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NO. NUMBER NO. REQUIRED
152D476X9050S2 4 -50A 1
2N1131 3 60 1
2N4398 3 75 1
2N696 3 145 2
2N696 4 15 1
212-12A 1 75 1
26S8-3 1 160 2
26S8-5 1 20 4
26S8-5 1 155 1
2600LW 1 25 4
2600LW 1 150 3
31882 2 -70
31882 3 -105
36151 2 -70A
36151 3 -105A
3810P102 3 70 1
4S3-78B 3 110 NP
43-03-1 3 -95
50FM256 2 15 2
55-0018-6 3 5 5
55-0018-6 4 40 2
55-0099-1 3 15 1
55-0225-15R05F 3 140 1
55-0225-90R03F 3 55 1
55-0290-4-11 3 160 1
55-0382-1011DS 3 135 1
55-0382-1021CS 3 30 4
55-0382-1031CS 3 45 1
55-0382-1055CS 4 25 1

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

Table 1001. Numeric Index (Sheet 5 of 7)

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NO. NUMBER NO. REQUIRED
55-0382-1531CS 3 25 1
55-0382-2015DS 3 115 1
55-0382-2241CS 3 185 1
55-0382-2711CS 3 165 1
55-0382-4711DS 3 10 2
55-0382-4715CS 3 155 1
55-0382-4715CS 4 30 1
55-0382-4721CS 3 170 1
55-0382-4725CS 4 35 1
55-0419-75R03F 2 5 1
55-0679-1051AF 3 50 3
55-0906-22553BR 4 5 1
55-0912-1 3 125 1
55-0912-1 4 10 1
55-2198-1 1 275 1
60-1321L1 1 310 1
60-1321L2 1 305 1
60-1321L3 1 320 1
60-1321-1 1 -1 RF
60-1321-1LB 1 -1A RF
60-1321-5 1 -1B RF
60-1321-5LB 1 -1C RF
60-1321-7 1 -1D RF
60-1321-7LB 1 -1E RF
60-1385-1 2 105 2
61-0320-1 1 5 NP
61-0457-1 1 -30 2
61-0457-5 1 -50 1
61-0458-1 1 -65 1
61-0459-1 2 115 1
61-0460-1 2 -125 1
61-0461-1 1 165 1

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

Table 1001. Numeric Index (Sheet 6 of 7)

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NO. NUMBER NO. REQUIRED
61-0462-1 1 110 1
61-0466-1 2 -85 1
61-0467-3 1 130 1
61-0468-3 1 -170 1
61-0470-1 2 95 1
61-0471-1 1 -120 1
61-0473-1 1 -15 1
61-0474-1 1 95 1
61-0475-1 1 -220
61-0476-1 1 -245
61-0477-1 1 -195
61-0478-1 1 -115
61-0478-9 1 -115A 1
61-0479-1 1 300 1
61-0479-1 2 -1 RF
61-0479-11 1 -300B 1
61-0479-11 2 -1B RF
61-0479-3 1 -300A 1
61-0479-3 2 -1A RF
61-0481-1 2 40 1
61-0482-1 1 -280
61-0482-5 1 -285 1
61-0485-1 2 160 1
61-0485-9 2 -160A 1
61-0488-1 1 10 NP
61-0532-1 1 190 2
61-2127-1 3 190 NP
61-2127-3 3 -190A NP
61-2128-1 2 20 1

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

Table 1001. Numeric Index (Sheet 7 of 7)

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NO. NUMBER NO. REQUIRED
61-2128-1 3 -1 RF
61-2128-13 2 -20B 1
61-2128-13 3 -1B RF
61-2128-7 2 -20A 1
61-2128-7 3 -1A RF
61-2838-1 1 315 1
61-2895-1 4 55 NP
61-2896-1 2 140 1
61-2896-1 4 -1 RF
61-3254-1 3 100 1
7717-158T 3 20 NP
7717-158T 3 65 NP
7717-158T 3 130 NP
7717-158T 3 150 NP
99N10-01A1 1 45 1
99R10-01A1 1 40 1

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

Emergency Exit Light Power Supply

IPL Figure 1

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Feb 1/06
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

FIG. & UNITS

ITEM AIRLINE NOMENCLATURE EFF PER
NO. PART NUMBER STOCK NO. 1 2 3 4 5 6 7 CODE ASSY

1 -1 60-1321-1 EMERGENCY EXIT LIGHT POWER SUPPLY A RF

-1A 60-1321-1LB EMERGENCY EXIT LIGHT POWER SUPPLY B RF
(LESS BATTERY)
-1B 60-1321-5 EMERGENCY EXIT LIGHT POWER SUPPLY C RF
-1C 60-1321-5LB EMERGENCY EXIT LIGHT POWER SUPPLY D RF
(LESS BATTERY)
-1D 60-1321-7 EMERGENCY EXIT LIGHT POWER SUPPLY E RF
-1E 60-1321-7LB EMERGENCY EXIT LIGHT POWER SUPPLY F RF
(LESS BATTERY)
R 5 61-0320-1 . PLATE, INSTRUCTION (SUPSD BY ITEM 305) NP
R 10 61-0488-1 . PLATE, IDENTIFICATION (SUPSD BY ITEM 310) NP
-15 61-0473-1 . COVER SUBASSEMBLY 1
20 26S8-5 . . STUD (V71286) (FA-390 - V72914) 4
25 2600LW . . WASHER (V71286) (TPN 2600-LW) 4
(FA-530 - V72914)
-30 61-0457-1 . . BRACKET ASSEMBLY 2
(ATTACHING PARTS)
35 MS24693S3 . . SCREW, FLAT HEAD (SUPSD BY ITEM -35A) NP
-35A MS24693S4 . . SCREW, FLAT HEAD (SUPSDS ITEM 35) NP
(SUPSD BY ITEM -35B)
-35B MS24693C4 . . SCREW, FLAT HEAD (SUPSDS ITEM -35A) 4
-------*-------
40 99R10-01A1 . . . RECEPTACLE (V71286) (FA-641 - V72914) 2
(ATTACHING PARTS)
45 99N10-01A1 . . . NUT, LOCK (V71286) (FA-642 - V72914) 2
-------*-------
-50 61-0457-5 . . . BRACKET SUBASSEMBLY 2
55 M45938-6-4 . . . . NUT, CLINCH (TPN M45938/6-4) 4
60 ORDER NHA . . . . BRACKET 1
-65 61-0458-1 . . BRACKET ASSEMBLY 1
(ATTACHING PARTS)
70 MS24693S3 . . SCREW, FLAT HEAD (SUPSD BY ITEM -70A) NP
-70A MS24693S4 . . SCREW, FLAT HEAD (SUPSDS ITEM 70) NP
(SUPSD BY ITEM -70B)
-70B MS24693C4 . . SCREW, FLAT HEAD (SUPSDS ITEM -70A) 2
-------*-------

- Item Not Illustrated

33-50-42 Page 1013

Feb 1/06
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

FIG. & UNITS

ITEM AIRLINE NOMENCLATURE EFF PER
NO. PART NUMBER STOCK NO. 1 2 3 4 5 6 7 CODE ASSY

1 75 212-12A . . . RECEPTACLE (V71286) (FA-540 - V72914) 1

(ATTACHING PARTS)
80 MS20426A3-5 . . . RIVET 2
-------*-------
85 M45938-6-4 . . . NUT, CLINCH (TPN M45938/6-4) 2
90 ORDER NHA . . . BRACKET NP
95 61-0474-1 . . HANDLE 1
(ATTACHING PARTS)
100 MS20426A4-5 . . RIVET 4
-------*-------
105 A2578 . . PLATE (TPN A-2578) (SUPSD BY ITEM -105A) NP
-105A A2578-3 . . PLATE (TPN A-2578-3) (SUPSDS ITEM 105) 2
110 61-0462-1 . . PLATE, COVER 1
-115 61-0478-1 . DELETED (REFER TO TIL NO. 232A)
-115A 61-0478-9 . BATTERY ASSEMBLY A,C,E 1
-120 61-0471-1 . . SUPPORT ASSEMBLY A,C,E 1
(ATTACHING PARTS)
125 MS35206-213 . . SCREW, PAN HEAD A,C,E 4
-------*-------
130 61-0467-3 . . . INSULATOR A,C,E 1
(ATTACHING PARTS)
135 MS35206-219 . . . SCREW, PAN HEAD A,C,E 1
140 AN960C4 . . . WASHER A,C,E 1
145 MS21042-04 . . . NUT, STOP A,C,E 1
-------*-------
150 2600LW . . . WASHER (V71286) (TPN 2600-LW) A,C,E 3
(FA-530 - V72914)
155 26S8-5 . . . STUD (V71286) A,C,E 1
(FA-390 - V72914)
160 26S8-3 . . . STUD (V71286) A,C,E 2
(FA-375 - V72914)
165 61-0461-1 . . . SUPPORT A,C,E 1
-170 61-0468-3 . . HOUSING ASSEMBLY A,C,E 1
(ATTACHING PARTS)
175 MS35190-226 . . SCREW, FLAT HEAD A,C,E 6
-------*-------

- Item Not Illustrated

33-50-42 Page 1014

Jul 1/00
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

FIG. & UNITS

ITEM AIRLINE NOMENCLATURE EFF PER
NO. PART NUMBER STOCK NO. 1 2 3 4 5 6 7 CODE ASSY

1 180 N41D188-440 . . . INSERT (V11815) (NS-050 - V72914) 3

185 ORDER NHA . . . HOUSING NP
190 61-0532-1 . . PAD, CUSHIONING A,C,E 2
-195 61-0477-1 . . DELETED (REFER TO TIL NO. 232A)
-200 MS35190-212 . . DELETED (REFER TO TIL NO. 232A)
-205 MS35649-222 . . DELETED (REFER TO TIL NO. 232A)
-210 MS35338-39 . . DELETED (REFER TO TIL NO. 232A)
-215 MS27183-2 . . DELETED (REFER TO TIL NO. 232A)
-220 61-0475-1 . . DELETED (REFER TO TIL NO. 232A)
-225 MS35190-212 . . DELETED (REFER TO TIL NO. 232A)
-230 MS35649-222 . . DELETED (REFER TO TIL NO. 232A)
-235 MS35338-39 . . DELETED (REFER TO TIL NO. 232A)
-240 MS27183-2 . . DELETED (REFER TO TIL NO. 232A)
-245 61-0476-1 . . DELETED (REFER TO TIL NO. 232A)
-250 MS35190-212 . . DELETED (REFER TO TIL NO. 232A)
-255 MS35649-222 . . DELETED (REFER TO TIL NO. 232A)
-260 MS35338-39 . . DELETED (REFER TO TIL NO. 232A)
-265 MS27183-2 . . DELETED (REFER TO TIL NO. 232A)
-270 S106 . . DELETED (REFER TO TIL NO. 232A)
275 55-2198-1 . . BATTERY ASSEMBLY (BT1) A,C,E 1
-280 61-0482-1 . . DELETED (REFER TO TIL NO. 232A)
-285 61-0482-5 . . HOUSING ASSEMBLY A,C,E 1
290 N41D188-440 . . . INSERT (V11815) (NS-050 - V72914) 7
295 ORDER NHA . . . HOUSING NP
300 61-0479-1 . HOUSING ASSEMBLY (SEE IPL FIGURE 2 A,B 1
FOR DETAILS)
-300A 61-0479-3 . HOUSING ASSEMBLY (SEE IPL FIGURE 2 C,D 1
FOR DETAILS)
-300B 61-0479-11 . HOUSING ASSEMBLY (SEE IPL FIGURE 2 E,F 1
FOR DETAILS)
R 305 60-1321L2 . LABEL, INSTRUCTION (SUPSDS ITEM 5) 1
R 310 60-1321L1 . LABEL, IDENTIFICATION (SUPSDS ITEM 10) 1
R 315 61-2838-1 . LABEL, STATIC CAUTION 1
R 320 60-1321L3 . LABEL, MOD 2

- Item Not Illustrated

33-50-42 Page 1015

Feb 1/06
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

Housing Assembly
IPL Figure 2

33-50-42 Page 1016

Jul 1/00
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

FIG. & UNITS

ITEM AIRLINE NOMENCLATURE EFF PER
NO. PART NUMBER STOCK NO. 1 2 3 4 5 6 7 CODE ASSY

2 -1 61-0479-1 HOUSING ASSEMBLY (SEE IPL FIGURE 1 FOR NHA) A RF

-1A 61-0479-3 HOUSING ASSEMBLY (SEE IPL FIGURE 1 FOR NHA) B RF
-1B 61-0479-11 HOUSING ASSEMBLY (SEE IPL FIGURE 1 FOR NHA) C RF
5 55-0419-75R03F . RESISTOR, 75 OHM, 10 W, 3% (R1) 1
(ATTACHING PARTS)
10 MS35206-203 . SCREW, PAN HEAD (SUPSD BY ITEM -10A) NP
-10A MS51957-3 . SCREW, PAN HEAD (SUPSDS ITEM 10) 2
15 50FM256 . NUT, STOP (V80539) (TPN 50FM-256) 2
(SN-484 - V72914)
-------*-------
20 61-2128-1 . PRINTED CIRCUIT CARD ASSEMBLY A 1
(SEE IPL FIGURE 3 FOR DETAILS)
-20A 61-2128-7 . PRINTED CIRCUIT CARD ASSEMBLY B 1
(SEE IPL FIGURE 3 FOR DETAILS)
-20B 61-2128-13 . PRINTED CIRCUIT CARD ASSEMBLY C 1
(SEE IPL FIGURE 3 FOR DETAILS)
(ATTACHING PARTS)
25 MS35206-216 . SCREW, PAN HEAD (SUPSD BY ITEM -25A) NP
-25A MS35206-217 . SCREW, PAN HEAD (SUPSDS ITEM 25) NP
(SUPSD BY ITEM -25B)
-25B MS51957-17 . SCREW, PAN HEAD (SUPSDS ITEM -25A) 4
30 MS21042-04 . NUT, STOP (SUPSD BY ITEM -30A) NP
-30A MS21042L04 . NUT, STOP (SUPSDS ITEM 30) 4
-------*-------
35 A3905 . SPACER (TPN A-3905) 4
40 61-0481-1 . INSULATOR 1
45 MS24264R12B12PX . CONNECTOR (J1) (SUPSD BY ITEM -45A) NP
-45A MS24264R12B12PN . CONNECTOR (J1) (SUPSDS ITEM 45) 1
(ATTACHING PARTS)
50 MS35206-213 . SCREW, PAN HEAD (SUPSD BY ITEM -50A) NP
-50A MS35206-214 . SCREW, PAN HEAD (SUPSDS ITEM 50) NP
(SUPSD BY ITEM -50B)
-50B MS51957-14 . SCREW, PAN HEAD (SUPSDS ITEM -50A) 4
55 MS21042-04 . NUT, STOP (SUPSD BY ITEM -55A) NP
-55A MS21042L04 . NUT, STOP (SUPSDS ITEM 55) 4
-------*-------

- Item Not Illustrated

33-50-42 Page 1017

Jul 1/00
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

FIG. & UNITS

ITEM AIRLINE NOMENCLATURE EFF PER
NO. PART NUMBER STOCK NO. 1 2 3 4 5 6 7 CODE ASSY

2 -60 M39029-31-241 . DELETED (MOVED TO REPAIR SECTION)

-65 MS27488-20 . DELETED (MOVED TO REPAIR SECTION)
-70 31882 . DELETED (MOVED TO REPAIR SECTION)
-70A 36151 . DELETED (MOVED TO REPAIR SECTION)
75 MS21042-06 . NUT, STOP 1
80 NAS620-6L . WASHER, FLAT 1
-85 61-0466-1 . TERMINAL ASSEMBLY 1
(ATTACHING PARTS)
90 MS24693S2 . SCREW, FLAT HEAD (SUPSD BY ITEM -90A) NP
-90A MS24693C2 . SCREW, FLAT HEAD (SUPSDS ITEM 90) 2
-------*-------
95 61-0470-1 . . PIN 1
(ATTACHING PARTS)
100 MS21042-06 . . NUT, STOP (SUPSD BY ITEM -100A) NP
-100A MS21042L06 . . NUT, STOP (SUPSDS ITEM 100) 1
-------*-------
105 60-1385-1 . . TERMINAL 2
110 121 . . PLUG, BANANA (V83330) (CO-719 - V72914) 2
115 61-0459-1 . . INSULATOR 1
(ATTACHING PARTS)
120 MS20426A3-6 . . RIVET 1
-------*-------
-125 61-0460-1 . . BRACKET ASSEMBLY 1
130 K7000-04-9 . . . NUT, CLINCH (V15653) (SN-122 - V72914) 2
135 ORDER NHA . . . BRACKET NP
140 61-2896-1 . CIRCUIT CARD ASSEMBLY (SEE IPL FIGURE 4 C 1
FOR DETAILS)
(ATTACHING PARTS)
145 MS35206-217 . SCREW, PAN HEAD (SUPSD BY ITEM -145A) C NP
-145A MS51957-17 . SCREW, PAN HEAD (SUPSDS ITEM 145) C 4
150 MS210404 . NUT, STOP (SUPSD BY ITEM -150A) C NP
-150A MS21042L04 . NUT, STOP (SUPSDS ITEM 150) C 4
-------*-------
155 A3905 . SPACER (TPN A-3905) C 4
160 61-0485-1 . HOUSING A,B 1
-160A 61-0485-9 . HOUSING C 1

- Item Not Illustrated

33-50-42 Page 1018

Jul 1/00
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

This page left blank intentionally.

33-50-42 Page 1019

Jul 1/00
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

REF ITEM REF ITEM REF ITEM REF ITEM

DES NUMBER DES NUMBER DES NUMBER DES NUMBER
CR1 175 Q1 145 R2, R3 10 R13 140
CR2, CR3 5 Q2 60 R4 25 R14 165
CR4 120 Q3 145 R5 30 R15 70
CR5-CR7 5 Q4 125 R6 185 R16 30
CR8 180 Q5 75 R7 30 R17 155
C1 50 R8 55 R21 30
C2 35 R9 115 SCR1 15
C3 40 R10 45 U1 160
C4, C5 50 R11 135
R12 170

Printed Circuit Card Assembly

IPL Figure 3

33-50-42 Page 1020

Oct 1/05
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

FIG. & UNITS

ITEM AIRLINE NOMENCLATURE EFF PER
NO. PART NUMBER STOCK NO. 1 2 3 4 5 6 7 CODE ASSY

3 -1 61-2128-1 PRINTED CIRCUIT CARD ASSEMBLY A RF

(SEE IPL FIGURE 2 FOR NHA)
-1A 61-2128-7 PRINTED CIRCUIT CARD ASSEMBLY B RF
(SEE IPL FIGURE 2 FOR NHA)
-1B 61-2128-13 PRINTED CIRCUIT CARD ASSEMBLY C RF
(SEE IPL FIGURE 2 FOR NHA)
5 55-0018-6 . DIODE (CR2, CR3, CR5-CR7) 5
10 55-0382-4711DS . RESISTOR, 470 OHM, 1/2 W, 10% (R2, R3) 2
15 55-0099-1 . RECTIFIER (SCR1) 1
20 7717-158T . PAD, MOUNTING (V13103) (TR-330 - V72914) NP
(USED UNDER ITEM 15)
(SUPSD BY ITEM -20A)
-20A M38527-08-041P . PAD, MOUNTING (USED UNDER ITEM 15) 1
(SUPSDS ITEM 20)
25 55-0382-1531CS . RESISTOR, 15 K OHM, 1/4 W, 10% (R4) 1
30 55-0382-1021CS . RESISTOR, 1 K OHM, 1/4 W, 10% 4
(R5, R7, R16, R21) (POST SB 60-1321-33-0028)
35 WMF1S47K . CAPACITOR, 0.047 µF, 100 V, 20% (V93790) 1
(CA-262 - V72914) (C2)
40 150D476X9035S2 . CAPACITOR, 47 µF, 35 V, 10% (V56289) 1
(CA-660 - V72914) (C3)
45 55-0382-1031CS . RESISTOR, 10 K OHM, 1/4 W, 10% (R10) 1
50 55-0679-1051AF . CAPACITOR, 1 µF, 50 V, 10% (C1, C4, C5) 3
55 55-0225-90R03F . RESISTOR, 90 OHM, 3 W, 3% (R8) 1
60 2N1131 . TRANSISTOR (V01295) (TR-130 - V72914) (Q2) 1
65 7717-158T . PAD, MOUNTING (V13103) (TR-330 - V72914) NP
(USED UNDER ITEM 60)
(SUPSD BY ITEM -65A)
-65A M38527-08-041P . PAD, MOUNTING (USED UNDER ITEM 60) 1
(SUPSDS ITEM 65)
70 3810P102 . POTENTIOMETER, 1 K OHM, 1 W (V96791) 1
(RH-235 - V72914) (R15)
75 2N4398 . TRANSISTOR (V04713) (TR-040 - V72914) (Q5) 1
(ATTACHING PARTS)
80 MS35206-229 . SCREW, PAN HEAD 2
-80A MS35206-230 . DELETED
85 MS35338-41 . WASHER, LOCK 2
90 MS21042-06 . NUT, SELF-LOCKING 2
-------*-------

- Item Not Illustrated

33-50-42 Page 1021

Jul 1/00
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

FIG. & UNITS

ITEM AIRLINE NOMENCLATURE EFF PER
NO. PART NUMBER STOCK NO. 1 2 3 4 5 6 7 CODE ASSY

3 -95 43-03-1 . DELETED

100 61-3254-1 . HEAT SINK (POST SB 60-1321-33-0028) 1
-105 31882 . DELETED
-105A 36151 . DELETED (MOVED TO REPAIR SECTION)
110 4S3-78B . TERMINAL (V86577) (TE-571 - V72914) NP
(SUPSD BY ITEM -110A THROUGH -110C)
-110A 10-401-2-01 . TERMINAL (V18310) (TE-571 - V72914) A 11
(SUPSDS ITEM 110)
-110B 10-401-2-01 . TERMINAL (V18310) (TE-571 - V72914) B 12
(SUPSDS ITEM 110)
-110C 10-401-2-01 . TERMINAL (V18310) (TE-571 - V72914) C 13
(SUPSDS ITEM 110)
115 55-0382-2015DS . RESISTOR, 200 OHM, 1/2 W, 5% (R9) 1
120 1N5231B . DIODE, 5.1 V, 500 MW, 5% (V04713) 1
(RC-625 - V72914) (CR4)
125 55-0912-1 . TRANSISTOR (Q4) 1
130 7717-158T . PAD, MOUNTING (V13103) (TR-330 - V72914) NP
(USED UNDER ITEM 125)
(SUPSD BY ITEM -130A)
-130A M38527-08-041P . PAD, MOUNTING (USED UNDER ITEM 125) 1
(SUPSDS ITEM 130)
135 55-0382-1011DS . RESISTOR, 100 OHM, 1/2 W, 10% (R11) 1
140 55-0225-15R05F . RESISTOR, 15 OHM, 3 W, 5% (R13) 1
145 2N696 . TRANSISTOR (V01295) (TR-110 - V72914) (Q1, Q3) 2
150 7717-158T . PAD, MOUNTING (V13103) (TR-330 - V72914) NP
(USED UNDER ITEM 145)
(SUPSD BY ITEM -150A)
-150A M38527-08-041P . PAD, MOUNTING (USED UNDER ITEM 145) 2
(SUPSDS ITEM 150)
155 55-0382-4715CS . RESISTOR, 470 OHM, 1/4 W, 5% (R17) 1
160 55-0290-4-11 . INTEGRATED CIRCUIT (U1) 1
165 55-0382-2711CS . RESISTOR, 270 OHM, 1/4 W, 10% (R14) 1
170 55-0382-4721CS . RESISTOR, 4.7 K OHM, 1/4 W, 10% (R12) 1
175 1N4385 . DIODE (V14433) (RC-455 - V72914) (CR1) 1
180 1N4385 . DIODE (V14433) (RC-455 - V72914) (CR8) B 1
185 55-0382-2241CS . RESISTOR, 220 K OHM, 1/4 W, 10% (R6) 1
190 61-2127-1 . BOARD, PRINTED WIRING (ORDER NHA) A,B NP
-190A 61-2127-3 . BOARD, PRINTED WIRING (ORDER NHA) C NP

- Item Not Illustrated

33-50-42 Page 1022

Jul 1/00
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

This page left blank intentionally.

33-50-42 Page 1023

Jul 1/00
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

REF ITEM REF ITEM REF ITEM REF ITEM

DES NUMBER DES NUMBER DES NUMBER DES NUMBER
CR9, CR10 45 C6 5 Q6 15 R18 35
CR11, CR12 40 C7 50 Q7 10 R19 30
R20 25

Circuit Card Assembly

IPL Figure 4

33-50-42 Page 1024

Jul 1/00
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 60-1321

FIG. & UNITS

ITEM AIRLINE NOMENCLATURE EFF PER
NO. PART NUMBER STOCK NO. 1 2 3 4 5 6 7 CODE ASSY

4 -1 61-2896-1 CIRCUIT CARD ASSEMBLY (SEE IPL FIGURE 2 RF

FOR NHA)
5 55-0906-22553BR . CAPACITOR, 2.2 µF, 135 V, 10% (C6) 1
10 55-0912-1 . TRANSISTOR (Q7) 1
15 2N696 . TRANSISTOR (V01295) (TR-110 - V72914) (Q6) 1
20 M38527-004N . PAD, MOUNTING (SUPSD BY ITEM -20A) NP
-20A M38527-02-004N . PAD, MOUNTING (TPN M38527/02-004N) 2
(SUPSDS ITEM 20)
25 55-0382-1055CS . RESISTOR, 1 M OHM, 1/4 W, 5% (R20) 1
30 55-0382-4715CS . RESISTOR, 470 OHM, 1/4 W, 5% (R19) 1
35 55-0382-4725CS . RESISTOR, 4.7 K OHM, 1/4 W, 5% (R18) 1
40 55-0018-6 . DIODE (CR11, CR12) 2
45 1N4385 . DIODE (V14433) (RC-455 - V72914) (CR9, CR10) 2
50 150D476X9035S2 . CAPACITOR, 47 µF, 35 V, 10% (V56289) NP
(CA-660 - V72914) (C7) (SUPSD BY ITEM -50A)
-50A 152D476X9050S2 . CAPACITOR, 47 µF, 50 V, 10% (V56289) 1
(CA-6638 - V72914) (C7)
(SUPSDS ITEM 50)
55 61-2895-1 . BOARD, PRINTED WIRING (ORDER NHA) NP

- Item Not Illustrated

33-50-42 Page 1025/1026

Jul 1/00